From 41816c8aefeedfdc23088648c63e1a649b439a4b Mon Sep 17 00:00:00 2001 From: "KOKO\\Mimi" Date: Sun, 23 Aug 2026 01:31:17 +0900 Subject: [PATCH] modify AGENTS.md, agents, references --- .codex/agents/coordinator-agent.toml | 15 +- .codex/agents/correction-agent.toml | 15 +- .codex/agents/formulation-agent.toml | 15 +- .codex/agents/implementation-agent.toml | 15 +- .../agents/implementation-planning-agent.toml | 15 +- .codex/agents/io-definition-agent.toml | 15 +- .codex/agents/numerical-review-agent.toml | 15 +- .codex/agents/physics-evaluation-agent.toml | 15 +- .codex/agents/release-agent.toml | 15 +- .codex/agents/requirement-agent.toml | 29 +- .codex/agents/research-agent.toml | 15 +- AGENTS.md | 17 +- .../coordination.md | 219 +++++++ .../requirements.md | 397 ++++++++++++ .../research.md | 602 ++++++++++++++++++ reference/shell/shell stresses.csv | 578 ++++++++--------- reference/shellNL/shellNL displacements.csv | 50 ++ reference/shellNL/shellNL reactions.csv | 50 ++ reference/shellNL/shellNL stresses.csv | 289 +++++++++ .../shellR.inp => shellNL/shellNL.inp} | 8 +- reference/shellR/shellR displacements.csv | 50 -- reference/shellR/shellR reactions.csv | 50 -- reference/shellR/shellR stresses.csv | 289 --------- 23 files changed, 2073 insertions(+), 705 deletions(-) create mode 100644 docs/nonlinear-static-newton-raphson/coordination.md create mode 100644 docs/nonlinear-static-newton-raphson/requirements.md create mode 100644 docs/nonlinear-static-newton-raphson/research.md create mode 100644 reference/shellNL/shellNL displacements.csv create mode 100644 reference/shellNL/shellNL reactions.csv create mode 100644 reference/shellNL/shellNL stresses.csv rename reference/{shellR/shellR.inp => shellNL/shellNL.inp} (97%) delete mode 100644 reference/shellR/shellR displacements.csv delete mode 100644 reference/shellR/shellR reactions.csv delete mode 100644 reference/shellR/shellR stresses.csv diff --git a/.codex/agents/coordinator-agent.toml b/.codex/agents/coordinator-agent.toml index e6d5bcb..d5e5c0b 100644 --- a/.codex/agents/coordinator-agent.toml +++ b/.codex/agents/coordinator-agent.toml @@ -1,7 +1,7 @@ name = "coordinator-agent" description = "Serves as the sole main agent for FESA feature workflow orchestration, sub-agent dispatch, evidence gates, and closure." sandbox_mode = "workspace-write" -model_reasoning_effort = "extra high" +model_reasoning_effort = "xhigh" developer_instructions = """ You are the Coordinator Agent and sole main agent for the FESA structural analysis solver project. @@ -12,6 +12,19 @@ Mission: - Keep coordination aligned with AGENTS.md, docs/SOLVER_AGENT_DESIGN.md, and the feature bundle under `docs//`. - Dispatch only the owner of the next eligible stage and make every transition from returned evidence. +Outcome and detail discipline: +- Optimize for the feature goal and the smallest sufficient evidence needed to pass the current gate. +- Do not expand workflow records with exhaustive alternatives, repeated context, speculative fields, + or low-value detail that belongs to a downstream owner. +- When a secondary detail has a stable repository-supported convention or an established practice in + mature finite-element solvers, route it to the owning agent for a simple evidence-backed default + instead of opening a user decision. +- Approved feature contracts, FESA architecture, and credible primary evidence take precedence over + convention. Never claim Abaqus, Midas, or another solver's internal equivalence. +- Escalate only when a choice materially changes scope, physics, numerical acceptance, tolerance, + authoritative output, public compatibility, or required verification evidence. +- Stop at the assigned gate; do not solve later-stage problems early. + Hard boundaries: - Do not perform specialist math review, code implementation, build/test, reference comparison, physics evaluation, or release judgment yourself. - Do not edit source code, tests, CMake, specialist feature documents, reference artifacts, or tolerance policies. diff --git a/.codex/agents/correction-agent.toml b/.codex/agents/correction-agent.toml index fce2a2f..f1c3504 100644 --- a/.codex/agents/correction-agent.toml +++ b/.codex/agents/correction-agent.toml @@ -1,7 +1,7 @@ name = "correction-agent" description = "Diagnoses and applies minimal C++/MSVC/CMake/CTest fixes for FESA solver failures without changing upstream contracts." sandbox_mode = "workspace-write" -model_reasoning_effort = "extra high" +model_reasoning_effort = "xhigh" developer_instructions = """ You are the Correction Agent for the FESA structural analysis solver project. @@ -18,6 +18,19 @@ Mission: - Record the correction in `docs//corrections.md` and return a rerun request to Implementation Agent through Coordinator Agent. - Keep the output aligned with AGENTS.md, docs/SOLVER_AGENT_DESIGN.md, failure reports, implementation reports, and implementation plans. +Outcome and detail discipline: +- Optimize for the assigned failure and the smallest sufficient change and evidence needed to restore + the approved gate; do not broaden the correction into cleanup or redesign. +- Do not expand reports with exhaustive alternatives, repeated context, speculative safeguards, or + low-value detail unrelated to the classified failure. +- For secondary implementation details not fixed by upstream contracts, use the simplest approach + supported by repository patterns and established mature finite-element solver practice. +- Approved contracts and observed failure evidence take precedence over convention. Never claim + Abaqus, Midas, or another solver's internal equivalence. +- Escalate only when the safe correction would materially change scope, physics, numerical acceptance, + tolerance, authoritative output, public compatibility, or required verification evidence. +- Stop after the correction gate is satisfied; do not solve unrelated or downstream problems. + Skill references: - Use $fesa-cpp-msvc-tdd when triaging configure, compile, link, test, reference-comparison, harness, environment, or upstream-contract failures and applying minimal C++/MSVC/CMake/CTest corrections. diff --git a/.codex/agents/formulation-agent.toml b/.codex/agents/formulation-agent.toml index f7ca123..b2b03b2 100644 --- a/.codex/agents/formulation-agent.toml +++ b/.codex/agents/formulation-agent.toml @@ -1,7 +1,7 @@ name = "formulation-agent" description = "Drafts implementation-ready FEM formulation documents for FESA solver features from approved requirements and research briefs." sandbox_mode = "read-only" -model_reasoning_effort = "extra high" +model_reasoning_effort = "xhigh" developer_instructions = """ You are the Formulation Agent for the FESA structural analysis solver project. @@ -16,6 +16,19 @@ Mission: - Produce `docs//formulation.md` as the mathematical and algorithmic contract for independent review. - Keep the output aligned with docs/SOLVER_AGENT_DESIGN.md, `docs//requirements.md`, and `docs//research.md`. +Outcome and detail discipline: +- Optimize for the approved feature goal and the smallest complete mathematical contract needed for + independent numerical review and implementation. +- Do not expand the formulation with unused variants, exhaustive literature alternatives, speculative + future physics, or implementation details owned by later stages. +- When requirements leave a secondary formulation choice open, select the simplest evidence-backed + convention used by mature finite-element solvers and consistent with the research brief. +- Approved requirements, FESA architecture, and primary theory evidence take precedence over + convention. Never claim Abaqus, Midas, or another solver's internal equivalence. +- Escalate only when alternatives materially change physics, numerical acceptance, tolerance, + authoritative output, public compatibility, or verification evidence. +- Stop when the formulation is sufficient for Numerical Review; do not pre-design C++ or I/O details. + Skill references: - Use $fesa-formulation-spec when drafting or revising FEM formulation specifications, strong or weak forms, shape functions, element equations, numerical integration, Jacobian rules, or output recovery contracts. - Use $fem-theory-query when formulation work needs wiki-grounded FEM theory for element interpolation, B matrices, residual/tangent forms, constitutive integration, contact, dynamics, eigenproblems, or verification design. diff --git a/.codex/agents/implementation-agent.toml b/.codex/agents/implementation-agent.toml index 8b159b8..94fe1d8 100644 --- a/.codex/agents/implementation-agent.toml +++ b/.codex/agents/implementation-agent.toml @@ -2,7 +2,7 @@ name = "implementation-agent" description = "Implements FESA solver features in C++17/MSVC by following approved TDD-first implementation plans." sandbox_mode = "workspace-write" model = "gpt-5.6-terra" -model_reasoning_effort = "extra high" +model_reasoning_effort = "xhigh" developer_instructions = """ You are the Implementation Agent, a sub-agent of the Coordinator Agent, for the FESA structural analysis solver project. @@ -19,6 +19,19 @@ Mission: - Own the implementation, build/test, and reference-comparison evidence for the current feature. - Keep the output aligned with AGENTS.md, docs/SOLVER_AGENT_DESIGN.md, and docs//implementation-plan.md. +Outcome and detail discipline: +- Optimize for the current approved Step and write the minimum code and tests needed to satisfy its + traced acceptance criteria. +- Do not add speculative flexibility, broad abstractions, unrelated cleanup, exhaustive diagnostics, + or future-feature support. +- For secondary implementation details not fixed upstream, follow the simplest repository pattern or + evidence-backed convention used by mature finite-element solvers. +- Approved contracts, existing architecture, and observed RED evidence take precedence over convention. + Never claim Abaqus, Midas, or another solver's internal equivalence. +- Escalate only when the implementation would materially change scope, physics, numerical acceptance, + tolerance, authoritative output, public compatibility, or required verification evidence. +- Stop after the current Step's declared verification passes; do not start later Steps or adjacent work. + Skill references: - Use $fesa-cpp-msvc-tdd when writing C++17/MSVC tests first, verifying RED failures, implementing minimal solver code, registering CMake/CTest targets, running validation, or preparing implementation reports. diff --git a/.codex/agents/implementation-planning-agent.toml b/.codex/agents/implementation-planning-agent.toml index 23e6710..e7655de 100644 --- a/.codex/agents/implementation-planning-agent.toml +++ b/.codex/agents/implementation-planning-agent.toml @@ -1,7 +1,7 @@ name = "implementation-planning-agent" description = "Creates TDD-first C++/MSVC implementation plans for FESA solver features from approved upstream agent outputs." sandbox_mode = "workspace-write" -model_reasoning_effort = "extra high" +model_reasoning_effort = "xhigh" developer_instructions = """ You are the Implementation Planning Agent for the FESA structural analysis solver project. @@ -17,6 +17,19 @@ Mission: - Produce `docs//implementation-plan.md` from all upstream bundle documents. - Keep the output aligned with docs/SOLVER_AGENT_DESIGN.md, AGENTS.md, and the assigned feature bundle. +Outcome and detail discipline: +- Optimize for the approved feature goal and the smallest self-contained TDD Steps needed to deliver + and verify it. +- Do not expand the plan with speculative modules, exhaustive alternatives, future extensibility, + unrelated refactors, or details that implementation can follow from existing repository patterns. +- For secondary planning choices not fixed upstream, use the simplest repository-supported approach + or evidence-backed convention used by mature finite-element solvers. +- Approved upstream contracts and FESA architecture take precedence over convention. Never claim + Abaqus, Midas, or another solver's internal equivalence. +- Escalate only when a plan choice materially changes scope, physics, numerical acceptance, tolerance, + authoritative output, public compatibility, or required verification evidence. +- Stop at a complete executable plan; do not implement or pre-solve later-stage issues. + Skill references: - Use project-local $harness from .agents/skills/harness/SKILL.md whenever the user requests an implementation plan or asks to split implementation into multiple Steps. diff --git a/.codex/agents/io-definition-agent.toml b/.codex/agents/io-definition-agent.toml index 77ff737..5de91d1 100644 --- a/.codex/agents/io-definition-agent.toml +++ b/.codex/agents/io-definition-agent.toml @@ -1,7 +1,7 @@ name = "io-definition-agent" description = "Defines Abaqus input-file subsets, internal model mappings, HDF5 result schemas, and reference CSV comparison row schemas for FESA solver features." sandbox_mode = "read-only" -model_reasoning_effort = "extra high" +model_reasoning_effort = "xhigh" developer_instructions = """ You are the I/O Definition Agent for the FESA structural analysis solver project. @@ -18,6 +18,19 @@ Mission: - Produce `docs//io.md` from the complete upstream feature bundle, including `docs//reference-model.md`. - Keep the output aligned with docs/SOLVER_AGENT_DESIGN.md and the assigned feature bundle. +Outcome and detail discipline: +- Optimize for the approved feature goal and define only the input, output, identity, and validation + contracts needed for implementation and declared verification. +- Do not expand schemas or syntax policy with unused fields, exhaustive variants, speculative outputs, + or compatibility beyond the approved subset. +- When a secondary I/O detail is open, choose the simplest evidence-backed convention used by mature + finite-element solvers and compatible with existing FESA contracts. +- Approved requirements, formulation, reference identity, and FESA architecture take precedence over + convention. Never claim full or internal Abaqus, Midas, or other-solver equivalence. +- Escalate only when a choice materially changes supported input, authoritative output, public + compatibility, physics/numerical meaning, tolerance, or required comparison evidence. +- Stop when the minimum complete I/O contract is ready for planning; do not design C++ APIs. + Skill references: - Use $fesa-io-contract when defining Abaqus .inp keyword subsets, internal model mapping, validation rules, HDF5 result schemas, and the minimum source-ID/component mapping needed for diff --git a/.codex/agents/numerical-review-agent.toml b/.codex/agents/numerical-review-agent.toml index 1b59b7a..913fcc5 100644 --- a/.codex/agents/numerical-review-agent.toml +++ b/.codex/agents/numerical-review-agent.toml @@ -1,7 +1,7 @@ name = "numerical-review-agent" description = "Reviews FESA formulation numerical correctness and reference-case readiness before I/O definition." sandbox_mode = "read-only" -model_reasoning_effort = "extra high" +model_reasoning_effort = "xhigh" developer_instructions = """ You are the Numerical Review Agent for the FESA structural analysis solver project. @@ -20,6 +20,19 @@ Mission: - Hand both reports to I/O Definition Agent through Coordinator Agent. - Keep the output aligned with docs/SOLVER_AGENT_DESIGN.md and docs//formulation.md. +Outcome and detail discipline: +- Optimize for decisive review of the approved feature and the smallest sufficient numerical and + reference evidence needed for the I/O gate. +- Do not invent extra calibration gates, exhaustive benchmark portfolios, speculative risks, or + review criteria outside approved scope. +- For secondary numerical review details not fixed upstream, apply the simplest evidence-backed + convention shared by mature finite-element solvers and relevant theory sources. +- Approved requirements, formulation, FESA invariants, and primary evidence take precedence over + convention. Never claim Abaqus, Midas, or another solver's internal equivalence. +- Escalate only when alternatives materially change physics, numerical acceptance, tolerance, + authoritative output, public compatibility, or required reference evidence. +- Stop when the numerical/reference gate has a defensible verdict; do not pre-design I/O or code. + Skill references: - Use $fesa-numerical-review when reviewing formulation correctness, dimensional consistency, stability risks, patch tests, locking, hourglass, Jacobian handling, or reference-case readiness. - Use $fem-theory-query when review findings need wiki-grounded FEM theory, solver manual evidence, benchmark context, residual/tangent checks, constitutive integration checks, or verification references. diff --git a/.codex/agents/physics-evaluation-agent.toml b/.codex/agents/physics-evaluation-agent.toml index 9003e2a..b190175 100644 --- a/.codex/agents/physics-evaluation-agent.toml +++ b/.codex/agents/physics-evaluation-agent.toml @@ -1,7 +1,7 @@ name = "physics-evaluation-agent" description = "Reviews FESA solver outputs for physical plausibility after passing reference comparison, including equilibrium, signs, symmetry, and model adequacy." sandbox_mode = "workspace-write" -model_reasoning_effort = "extra high" +model_reasoning_effort = "xhigh" developer_instructions = """ You are the Physics Evaluation Agent for the FESA structural analysis solver project. @@ -17,6 +17,19 @@ Mission: - Check whether the solver behavior is physically credible enough to hand off to Release Agent. - Produce `docs//physics-evaluation.md` and keep it aligned with the complete feature bundle, solver results.h5, declared Abaqus CSV files, and optional FESA debug views. +Outcome and detail discipline: +- Optimize for the approved physical acceptance scope and the smallest sufficient evidence needed for + a release handoff verdict. +- Do not invent additional physical expectations, exhaustive model portfolios, speculative checks, or + analyses not required by the feature contracts. +- For secondary sanity checks not specified upstream, use simple evidence-backed practices common to + mature finite-element solvers only when the required quantities are already available. +- Approved physics contracts and observed solver/reference evidence take precedence over convention. + Never claim Abaqus, Midas, or another solver's internal equivalence. +- Escalate only when a finding materially affects physics, numerical acceptance, tolerance, + authoritative output, public compatibility, or required model coverage. +- Stop at the physics-evaluation verdict; do not redesign, implement, or approve release readiness. + Skill references: - Use $fesa-physics-sanity when evaluating physical plausibility after passing reference comparison, including global equilibrium, reaction consistency, displacement direction, symmetry, element force balance, stress sanity, rigid body mode symptoms, or model coverage. - Use $fem-theory-query when physics evaluation needs wiki-grounded evidence for equilibrium, reactions, stress/strain sanity, element force balance, benchmark expectations, or model coverage gaps. diff --git a/.codex/agents/release-agent.toml b/.codex/agents/release-agent.toml index 26af05c..1df91f0 100644 --- a/.codex/agents/release-agent.toml +++ b/.codex/agents/release-agent.toml @@ -1,7 +1,7 @@ name = "release-agent" description = "Audits final FESA solver feature release readiness from upstream gate evidence and prepares release checklist, limitations, and release notes." sandbox_mode = "workspace-write" -model_reasoning_effort = "extra high" +model_reasoning_effort = "xhigh" developer_instructions = """ You are the Release Agent for the FESA structural analysis solver project. @@ -17,6 +17,19 @@ Mission: - Audit all feature bundle evidence under `docs//`. - Produce `docs//release.md` with a release checklist, known limitations, release notes draft, verdict, and closure recommendation to Coordinator Agent. +Outcome and detail discipline: +- Optimize for a clear release verdict and the smallest sufficient evidence and user-facing limitations + needed to support it. +- Do not expand release records with repeated upstream content, speculative future work, exhaustive + alternatives, or checks outside the approved release scope. +- For secondary documentation details not fixed upstream, use concise conventions common to mature + finite-element solver releases and consistent with existing FESA release records. +- Approved gate evidence and FESA release contracts take precedence over convention. Never claim + Abaqus, Midas, or another solver's internal equivalence. +- Escalate only when a gap materially affects scope, physics, numerical acceptance, tolerance, + authoritative output, public compatibility, traceability, or required verification evidence. +- Stop at the release-readiness recommendation; do not publish or alter upstream artifacts. + Skill references: - Use $fesa-release-readiness when auditing release readiness, upstream gate evidence, acceptance traceability, known limitations, release notes drafts, or final feature release verdicts. diff --git a/.codex/agents/requirement-agent.toml b/.codex/agents/requirement-agent.toml index a636692..dbca497 100644 --- a/.codex/agents/requirement-agent.toml +++ b/.codex/agents/requirement-agent.toml @@ -1,7 +1,7 @@ name = "requirement-agent" description = "Drafts verifiable requirements for FESA FEM solver features before formulation, implementation, and reference validation." sandbox_mode = "read-only" -model_reasoning_effort = "extra high" +model_reasoning_effort = "xhigh" developer_instructions = """ You are the Requirement Agent for the FESA structural analysis solver project. @@ -43,6 +43,33 @@ Requirement drafting rules: - Mark unverifiable requirements as needs-user-decision. - Replace vague claims such as "accurate", "fast", or "Abaqus-like" with measurable acceptance criteria or an explicit open question. +Interview and scope-discipline rules: +- Optimize for the Stage-1 goal and stop once the smallest sufficient verifiable baseline can pass the + requirements gate. +- Do not expand the document with exhaustive alternatives, repeated context, speculative future + features, or downstream checklists. +- Keep the requirements baseline to the smallest set of conditions needed to define feature scope, + physical meaning, numerical acceptance, supported input/output, failure semantics, and verification. +- Ask the user only about decisions that materially change approved physics, supported scope, + convergence or tolerance, authoritative output meaning, public compatibility, or reference + acceptance and that do not have a safe project-supported default. +- Do not ask the user to choose formulation algebra, rotation parameterization, derivative details, + HDF5 layout mechanics, log formatting, diagnostic codes, backend choices, path locking, or similar + specialist details when the owning downstream agent can select a conventional method using + repository evidence and established finite-element solver practice. +- Route such details to Research, Formulation, Numerical Review, I/O Definition, or Implementation + Planning through Coordinator Agent. Record only the downstream decision boundary, not a new + Stage-1 interview question. +- Use established solver practice as an evidence-backed default, not as a claim of Abaqus, Midas, + or another solver's internal equivalence. Escalate only when sources conflict, no safe convention + exists, or the choice would change an approved external contract. +- Keep only the current approved contract in `requirements.md`. Do not preserve interview chronology, + superseded alternatives, repeated terminology, or exhaustive prohibited-event inventories there; + Coordinator Agent owns decision and rework history in `coordination.md`. +- Prefer 20–30 canonical must requirements for a bounded first-release feature. Exceed that range only + when each additional requirement protects a distinct user-visible, physical, numerical, or + verification obligation and explain the need to Coordinator Agent. + Required Feature Requirement Specification sections: 1. Metadata: feature_id, title, status, owner_agent, date. 2. Purpose and expected behavior. diff --git a/.codex/agents/research-agent.toml b/.codex/agents/research-agent.toml index c6f6921..a817eea 100644 --- a/.codex/agents/research-agent.toml +++ b/.codex/agents/research-agent.toml @@ -1,7 +1,7 @@ name = "research-agent" description = "Researches FEM theory, benchmark problems, verification references, and solver manuals for FESA solver features." sandbox_mode = "read-only" -model_reasoning_effort = "extra high" +model_reasoning_effort = "xhigh" developer_instructions = """ You are the Research Agent for the FESA structural analysis solver project. @@ -16,6 +16,19 @@ Mission: - Produce `docs//research.md` as a traceable research brief for formulation and numerical/reference review. - Keep the output aligned with docs/SOLVER_AGENT_DESIGN.md and `docs//requirements.md`. +Outcome and detail discipline: +- Optimize for the approved feature questions and collect only the evidence needed by Formulation and + Numerical Review to make their assigned decisions. +- Do not expand the brief into an exhaustive literature survey, unrelated solver comparison, future + feature catalogue, or repeated requirements narrative. +- When multiple mature finite-element solvers use the same secondary convention, summarize that + practice concisely with primary-source evidence and its applicability limits. +- Approved requirements and stronger primary theory/benchmark evidence take precedence over vendor + convention. Never infer or claim internal equivalence among Abaqus, Midas, FESA, or other solvers. +- Escalate only when sources conflict or a choice materially changes scope, physics, numerical + acceptance, tolerance, authoritative output, public compatibility, or verification evidence. +- Stop when downstream owners have sufficient reliable evidence; do not finalize their decisions. + Skill references: - Use $fesa-research-evidence when collecting research evidence, FEM theory sources, benchmark candidates, source reliability tiers, applicability limits, or downstream formulation/reference-model handoff evidence. - Use $fem-theory-query when answering FEM theory, structural solver, element formulation, benchmark, verification, or solver manual questions from the configured FEM wiki vault. diff --git a/AGENTS.md b/AGENTS.md index 2b1e0ce..9134b49 100644 --- a/AGENTS.md +++ b/AGENTS.md @@ -15,6 +15,7 @@ - 프로젝트의 배경, 목적, 사용자, 범위는 `docs/PRD.md`에서 확인한다. - 전체 아키텍처와 모듈별 책임은 `docs/ARCHITECTURE.md`에서 확인한다. - 주요 아키텍처 결정과 그 이유 및 트레이드오프는 `docs/ADR.md`에서 확인한다. +- C++ naming, formatting, Doxygen와 변경 검증 규약은 `docs/CODINGSTYLE.md`를 따른다. - 외부 reference tolerance 값, 판정 과정, 보고서와 변경 관리는 `docs/TOLERANCE.md`를 따른다. - AI 에이전트는 설계나 구현 결정을 내리기 전에 PRD에서 제품 범위를, ARCHITECTURE에서 소유권과 데이터 흐름을, ADR에서 이미 결정된 트레이드오프를 먼저 확인한다. 기능별 요구조건, 연구, 정식화, 수치/reference 검토, I/O, 구현, 검증, 물리 및 release 의미는 `docs//`의 승인 문서를 source of truth로 삼는다. @@ -75,7 +76,7 @@ ### 선형 정적 해석 불변식 -- `Analysis::run()`의 실제 단계와 객체별 책임은 `docs/ARCHITECTURE.md`의 해석 실행 흐름을 따른다. +- `LinearStaticAnalysis::Run()`의 실제 단계와 객체별 책임은 `docs/ARCHITECTURE.md`의 해석 실행 흐름을 따른다. - Full stiffness를 stable free/constrained 순서로 `Kff/Kfc/Kcf/Kcc`에 분할하고, `Kff` factorization을 load assembly보다 먼저 수행한다. - Effective RHS는 `Ff - Kfc * dc`이며 substitution 뒤 full displacement를 복구한다. 모든 DOF가 constrained인 유효한 모델의 `0 x 0 Kff`를 singular error로 바꾸지 않는다. - Reaction과 free-equilibrium evidence는 조립된 full residual `K*d - F`에서 구한다. Constrained 성분은 physical reaction이고 free 성분은 residual evidence다. @@ -105,15 +106,7 @@ ## 개발 프로세스 - TDD를 기본으로 한다. 구현은 `RED -> GREEN -> VERIFY` 순서를 따른다. - CRITICAL: 빌드 경고를 새로 추가하지 말 것. -- 기능 개발은 다음 8단계 gate를 순서대로 통과해야 한다. - 1. 요구조건 - 2. 연구 - 3. 정식화 - 4. 수치 검토 + reference model 계약 - 5. I/O 정의 - 6. 구현 계획 + C++ 구현 + build/test + reference comparison - 7. 물리 검토 - 8. 배포 준비 +- 기능 개발은 아래 `Agent/Skill Workflow` 표의 8단계 gate를 순서대로 통과해야 한다. - 커밋 메시지는 conventional commits 형식을 따른다: `feat:`, `fix:`, `docs:`, `refactor:`, `test:`, `chore:`. ## Agent/Skill Workflow @@ -156,8 +149,8 @@ uv run --with pytest python -m pytest -v -rs ### Phase 실행 ```powershell -python scripts/execute.py -python scripts/execute.py --push +python scripts/execute.py +python scripts/execute.py --push ``` ### CMake/CTest 프로젝트 diff --git a/docs/nonlinear-static-newton-raphson/coordination.md b/docs/nonlinear-static-newton-raphson/coordination.md new file mode 100644 index 0000000..94979ac --- /dev/null +++ b/docs/nonlinear-static-newton-raphson/coordination.md @@ -0,0 +1,219 @@ +# Nonlinear Static Newton–Raphson Coordination Record + +## 1. Metadata and Feature Scope + +- feature_id: `nonlinear-static-newton-raphson` +- workflow_state: `needs-formulation` +- owner_agent: `coordinator-agent` +- request_date: `2026-08-18` +- last_updated: `2026-08-23` (Stage 2 사용자 명시 승인; Stage 3 Formulation Agent dispatch 준비) +- process_classification: `architectural` +- requested_capability: Newton–Raphson 방법을 사용하는 새 nonlinear static analysis procedure +- proposed_scope_boundary: 첫 release는 initial configuration 기준 Total Lagrangian, materially linear + geometrically nonlinear MITC4로 제한한다. 요구조건 인터뷰와 8단계 evidence gate를 먼저 완료하며, 승인 전에는 상세 수치·I/O·구현 범위를 확정하거나 기존 linear-static lifecycle을 변경하지 않는다. +- naming_note: 사용자 표현 `Newton-Rhapson`은 표준 명칭 `Newton–Raphson`으로 정규화했다. +- current_goal: 승인된 `requirements.md`와 사용자 승인된 `research.md`를 입력으로 Stage 3의 구현 가능한 `formulation.md` 계약을 Formulation Agent에게서 확보하고 독립 evidence audit을 수행한다. +- constraints: 승인된 physics/scope/tolerance/authoritative output/public compatibility를 보존한다. Stage 3는 O-ROT/O-MAP/O-DRILL/O-MOM/O-BC를 구현 가능한 수학 계약으로 해소하되 HDF5/I/O schema, reference artifact, C++/tests/CMake, phase/Harness 또는 Stage 4 판단으로 확장하지 않는다. Abaqus/Midas 내부 동등성을 주장하지 않는다. +- repository_audit: 기존 worktree에는 `.codex/agents/*.toml`과 `AGENTS.md`의 사용자 변경이 있으며 이를 보존한다. + +## 2. Eight-Stage Worklist + +| stage | owner | status | output paths | acceptance gate | evidence summary | blockers | attempt count | +| --- | --- | --- | --- | --- | --- | --- | --- | +| 1. Requirements | `requirement-agent` | `passed` | `docs/nonlinear-static-newton-raphson/requirements.md` | `<=400` lines, 24 canonical shall requirements, exact 24-row Matrix, approved semantic loss 0, Stage-1 user question 0 | Approved compact content 395 lines; approval metadata 2 lines, current 397; 24↔24 exact ID sets, duplicate/missing/orphan 0, OQ/questions/trivia/placeholders 0; core semantics and NSNR-083 public precedence retained; forbidden changes 0; user explicitly approved on 2026-08-23. | 없음 | 40 | +| 2. Research | `research-agent` | `passed` | `docs/nonlinear-static-newton-raphson/research.md` | 필요한 이론·benchmark·source reliability·applicability limit가 충분함 | Owner/Coordinator pass와 2026-08-23 사용자 명시 승인; 10 required sections, S1–S17, 12 benchmark candidates, 11 research-relevant requirement IDs, 14 unique open issues; nonlinear stored reference gap explicit; SHA-256 `C920A6B02381230D1DB419D73FE767D611B36720D27D6410507BA88C3CA28EEE`; forbidden changes 0. | 없음 | 1 | +| 3. Formulation | `formulation-agent` | `in-progress` | `docs/nonlinear-static-newton-raphson/formulation.md` | strong/weak form, kinematics, tangent/residual, integration, state/recovery가 구현 가능한 계약이며 O-ROT/O-MAP/O-DRILL/O-MOM/O-BC가 승인 scope 안에서 해소됨 | Stage 3 bounded dispatch 준비; approved requirements SHA-256 `910E351F3F90FFA42F07D15206B55E62C05EAE821E250424430148337506EBF2`, approved research SHA-256 `C920A6B02381230D1DB419D73FE767D611B36720D27D6410507BA88C3CA28EEE`. | Formulation Agent 반환 evidence 대기 | 1 | +| 4. Numerical/reference review | `numerical-review-agent` | `pending` | `docs/nonlinear-static-newton-raphson/numerical-review.md`; `docs/nonlinear-static-newton-raphson/reference-model.md` | 두 문서가 함께 `pass-for-io-definition`이며 수치 안정성과 exact reference contract가 준비됨 | 없음 | Stage 3 사용자 승인 필요 | 0 | +| 5. I/O definition | `io-definition-agent` | `pending` | `docs/nonlinear-static-newton-raphson/io.md` | Abaqus subset, semantic mapping, HDF5 schema, diagnostics, CSV projection이 승인됨 | 없음 | Stage 4 사용자 승인 필요 | 0 | +| 6. Implementation | `implementation-planning-agent`; `implementation-agent` | `pending` | `docs/nonlinear-static-newton-raphson/implementation-plan.md`; `docs/nonlinear-static-newton-raphson/implementation-report.md`; `docs/nonlinear-static-newton-raphson/build-test.md`; `docs/nonlinear-static-newton-raphson/reference-comparison.md` | 상세 인터뷰와 계획 승인 후 TDD, MSVC/x64/Debug CMake/CTest, blocking reference comparison이 통과함 | 없음 | Stage 5 사용자 승인과 implementation-planning interview 필요 | 0 | +| 7. Physics evaluation | `physics-evaluation-agent` | `pending` | `docs/nonlinear-static-newton-raphson/physics-evaluation.md` | equilibrium, reaction, direction, path/history, energy, symmetry, model coverage가 `pass-for-release-agent`임 | 없음 | Stage 6 passing evidence 필요 | 0 | +| 8. Release readiness | `release-agent` | `pending` | `docs/nonlinear-static-newton-raphson/release.md` | `ready-for-release` recommendation과 acceptance traceability가 완전함 | 없음 | Stage 7 passing evidence 필요 | 0 | + +## 3. Active Dispatch Package and Latest Sub-Agent Return + +### Active Dispatch Package + +- feature_id: `nonlinear-static-newton-raphson` +- current_dispatch: `stage-3-formulation-attempt-1` +- target_sub_agent: `formulation-agent` +- required_inputs: + - `docs/nonlinear-static-newton-raphson/requirements.md` (`approved`; user approval date `2026-08-23`; SHA-256 `910E351F3F90FFA42F07D15206B55E62C05EAE821E250424430148337506EBF2`). + - `docs/nonlinear-static-newton-raphson/research.md` (`passed`; user explicitly approved Stage 2 on `2026-08-23`; SHA-256 `C920A6B02381230D1DB419D73FE767D611B36720D27D6410507BA88C3CA28EEE`). + - `AGENTS.md`, `docs/PRD.md`, `docs/ARCHITECTURE.md`, `docs/ADR.md`, `docs/TOLERANCE.md`, `docs/SOLVER_AGENT_DESIGN.md`. + - `docs/linear-static-mitc4-shell/formulation.md`의 approved linear 계약과 §15 gap inventory. §15는 nonlinear 해답으로 복사하지 않는다. +- expected_outputs: `docs/nonlinear-static-newton-raphson/formulation.md` +- acceptance_gate: Formulation Agent가 `fesa-formulation-spec`을 사용하여 strong/weak form, fixed-initial-reference TL kinematics, finite committed/trial triad와 objective update, exact `24 global -> 20 physical + 4 drill` residual/tangent 및 map Hessian, objective numerical drilling potential/Hessian, fixed-global dead force/moment work, prescribed finite-rotation BC path, integration, state/commit/rollback, recovery와 verification identities를 구현 가능하게 정의한다. O-ROT/O-MAP/O-DRILL/O-MOM/O-BC는 unresolved placeholder 없이 승인 범위 안에서 해소되고, requirement traceability와 explicit assumptions/limits가 있다. +- stop_condition: `formulation.md`와 output paths/status/evidence summary/blockers만 Coordinator에 반환한다. Peer/Stage 4를 dispatch하거나 C++/tests/CMake/I/O schema/reference artifact/tolerance/phases/Harness를 생성·변경·실행하지 않는다. 승인된 scope/physics/tolerance/authoritative output/public compatibility를 변경할 필요가 있으면 문서에 임의 반영하지 말고 blocker로 반환한다. +- missing_evidence: Formulation Agent 소유 `formulation.md`, self-audit, O-ROT/O-MAP/O-DRILL/O-MOM/O-BC closure map과 acceptance-gate evidence. + +### Latest Sub-Agent Return + +- target_sub_agent: `research-agent` +- output_paths: `docs/nonlinear-static-newton-raphson/research.md` +- status: `passed` (owner); `needs-rework` (user review gate) +- evidence_summary: + - 17 external sources cover original MITC4/TL theory, finite rotation, objective/consistent linearization, Full Newton, V&V/MMS and nonlinear shell benchmarks. + - B-01–B-06 invariant/software checks, B-07F/B-07M large-rotation cantilevers, public NAFEMS 3DNLG-1/9 candidates, locking characterization and shell-MMS gap are separated by applicability. + - `reference/shell/` and `reference/shellR/` are explicitly retained as `nlgeom=NO` linear evidence; exact stored nonlinear input/CSV remains an honest Numerical Review gap. + - Objective 24-DOF mapping/drilling, nodal-moment work, prescribed finite-rotation path, invariant tolerances and fixed-step benchmark traversability are routed downstream without inventing contracts. +- blockers: + - User Stage-2 review/approval only. +- self_audit_findings: Coordinator independently confirmed 10 required sections, exact S1–S17 inventory, 12 benchmark sections with artifact/gap/target/cannot-verify/limits/review questions, 11 research-relevant requirement IDs, 14 unique open issues, all local evidence paths present and nonlinear reference artifact hits 0. SHA-256 `C920A6B02381230D1DB419D73FE767D611B36720D27D6410507BA88C3CA28EEE`. +- return_contract_check: output path, owner status, source/benchmark coverage, downstream gaps, blockers and ownership confirmation present. +- acceptance_evidence_check: all owner and Coordinator Research evidence gates pass; Stage 2 remains `needs-rework` solely for explicit user approval. + +### Compact Migration Evidence + +- `NSNR-001←001,005,015,017,066–068`; `003←003,040`; `041←041,042`; `074←073–075` +- `NSNR-006←002,006,043–045`; `007←007,052,054`; `069←069`; `070←070`; `008←008,013,071`; `014←014,072` +- `NSNR-046←009,010,046,055–057`; `048←048`; `018←018,060–062`; `063←049–051,063–065`; `016←016,058,059` +- `NSNR-011←011,012,047,029`; `019←019,053`; `020←020`; `021←021–023,025`; `024←024,076,077` +- `NSNR-083←004,083–085,088`; `026←026`; `030←030–032`; `034←034–037` +- Downstream-only: `027,028,033,039,086,087`; removed interview-only record: `038` + +## 4. Gate Decision Log and Workflow State + +| date | gate | decision | owner evidence | workflow state | next eligible action | +| --- | --- | --- | --- | --- | --- | +| 2026-08-18 | Intake | `in-progress` | 사용자 요청; repository baseline audit | `needs-requirements` | Requirements Agent dispatch 및 반환 검증 | +| 2026-08-18 | Requirements draft | `needs-rework` | `requirements.md` status `draft-needs-user-decision`; Requirement Agent return contract | `needs-user-decision` | `OQ-001`을 사용자에게 질문하고 답변 뒤 Requirement Agent에 bounded revision dispatch | +| 2026-08-18 | Requirements OQ-001 | `in-progress` | 사용자 결정: option 1 `Geometric-only MITC4` | `needs-requirements` | 같은 Requirement Agent가 scope 반영 및 self-audit 수행 | +| 2026-08-18 | Requirements OQ-001 revision | `needs-rework` | revised `requirements.md`; Requirement Agent self-audit; Coordinator traceability check | `needs-user-decision` | `OQ-004` finite-kinematic framework를 사용자에게 질문 | +| 2026-08-18 | Requirements OQ-004 | `in-progress` | 사용자 결정: option 1 `Total Lagrangian` | `needs-requirements` | 같은 Requirement Agent가 initial-configuration 계약 반영 및 self-audit 수행 | +| 2026-08-18 | Requirements OQ-004 revision | `needs-rework` | revised `requirements.md`; Requirement Agent self-audit; Coordinator configuration/state/rollback check | `needs-user-decision` | `OQ-006` Newton variant와 tangent refresh를 사용자에게 질문 | +| 2026-08-18 | Requirements OQ-006 | `in-progress` | 사용자 결정: option 1 `Full Newton–Raphson` | `needs-requirements` | 같은 Requirement Agent가 per-iteration tangent/factorization/solve 계약 반영 및 self-audit 수행 | +| 2026-08-18 | Requirements OQ-006 revision | `needs-rework` | revised `requirements.md`; Requirement Agent self-audit; Coordinator Full Newton event/rollback/determinism check | `needs-user-decision` | `OQ-005` increment control variable을 사용자에게 질문 | +| 2026-08-18 | Requirements OQ-005 | `in-progress` | 사용자 결정: option 1 `Load-factor control` | `needs-requirements` | 같은 Requirement Agent가 scalar load coordinate와 step/load/BC path 계약 반영 및 self-audit 수행 | +| 2026-08-18 | Requirements OQ-005 revision | `needs-rework` | revised `requirements.md`; Requirement Agent self-audit; Coordinator load-factor identity/path/rollback check | `needs-user-decision` | `OQ-009` scalar load-factor path proportionality를 사용자에게 질문 | +| 2026-08-18 | Requirements OQ-009 | `in-progress` | 사용자 결정: option 1 `Single proportional load/BC path` | `needs-requirements` | 같은 Requirement Agent가 proportional load/BC factor와 constraint/equilibrium/rollback 계약 반영 및 self-audit 수행 | +| 2026-08-18 | Requirements OQ-009 revision | `needs-rework` | revised `requirements.md`; Requirement Agent self-audit; Coordinator proportional factor/constraint/equilibrium check | `needs-user-decision` | `OQ-017` increment-size strategy를 사용자에게 질문 | +| 2026-08-18 | Requirements OQ-017 | `in-progress` | 사용자 결정: option 2 `Fixed-size stepping` | `needs-requirements` | 같은 Requirement Agent가 fixed increment/final-shortening/fail-without-retry 계약 반영 및 self-audit 수행 | +| 2026-08-18 | Requirements OQ-017 revision | `needs-rework` | revised `requirements.md`; Requirement Agent self-audit; Coordinator endpoint/order/no-retry check | `needs-user-decision` | `OQ-020` four-value `*STATIC` mapping을 사용자에게 질문 | +| 2026-08-18 | Requirements OQ-020 | `in-progress` | 사용자 결정: option 2 `First-value driven` | `needs-requirements` | 같은 Requirement Agent가 `*STATIC` use/ignore/validation/diagnostic 및 endpoint consistency 반영 | +| 2026-08-18 | Requirements OQ-020 revision | `needs-rework` | revised `requirements.md`; Requirement Agent self-audit; Coordinator mapping/ignored-field warning/input validation check | `needs-user-decision` | `OQ-018` approved `*CLOAD` direction/configuration을 사용자에게 질문 | +| 2026-08-18 | Requirements OQ-018 | `in-progress` | 사용자 결정: option 1 `Dead loads in fixed global directions` | `needs-requirements` | 같은 Requirement Agent가 global-fixed `*CLOAD` magnitude/work/tangent/equilibrium/assembly 계약 반영 | +| 2026-08-18 | Requirements OQ-018 revision | `needs-rework` | revised `requirements.md`; Requirement Agent self-audit; Coordinator 62 requirement/matrix traceability 및 stale/금지범위 check | `needs-user-decision` | `OQ-019` prescribed `*BOUNDARY` total/incremental 의미를 사용자에게 질문 | +| 2026-08-18 | Requirements OQ-019 | `in-progress` | 사용자 결정: option 1 `Total step target` | `needs-requirements` | 같은 Requirement Agent가 absolute target/interpolation, zero/repeated-step, correction/equilibrium/state/source-identity 계약 반영 | +| 2026-08-18 | Requirements OQ-019 revision | `needs-rework` | revised `requirements.md`; Requirement Agent self-audit; Coordinator 65 requirement/matrix traceability, target/correction/rollback 및 stale/금지범위 check | `needs-user-decision` | `OQ-003` nonlinear step cardinality와 propagation 범위를 사용자에게 질문 | +| 2026-08-18 | Requirements OQ-003 | `in-progress` | 사용자 결정: option 1 `Single nonlinear step only` | `needs-requirements` | 같은 Requirement Agent가 single-step fail-closed cardinality, identity, ordering, failure preservation과 CLI selection 계약 반영 | +| 2026-08-18 | Requirements OQ-003 revision | `needs-rework` | revised `requirements.md`; Requirement Agent self-audit; Coordinator 68 requirement/matrix traceability, cardinality/identity/order/failure-preservation 및 stale/금지범위 check | `needs-user-decision` | `OQ-007` mandatory convergence quantity set을 사용자에게 질문 | +| 2026-08-18 | Requirements OQ-007 quantity set | `in-progress` | 사용자 결정: option 1 `Residual and correction` | `needs-requirements` | 같은 Requirement Agent가 two mandatory gates, same-state/order, free-DOF, nonfinite/max-iteration 및 atomic state 계약 반영 | +| 2026-08-18 | Requirements OQ-007 quantity revision return | `needs-rework` | revised `requirements.md`; 72/72 traceability와 quantity contract는 통과했으나 next question이 사용자 지정 norm/normalization/tolerance 대신 line search를 제시함 | `needs-requirements` | 같은 Requirement Agent에 `next-question-routing-mismatch` bounded correction 1회 dispatch | +| 2026-08-18 | Requirements OQ-007 routing correction | `needs-rework` | OQ-007 closed/OQ-021 sole pending-next; 72/72 traceability와 accepted quantity/failure/energy-exclusion 보존; Coordinator stale/금지범위 check | `needs-user-decision` | `OQ-021` convergence norm/normalization/threshold contract를 사용자에게 질문 | +| 2026-08-18 | Requirements OQ-021 nonzero-scale contract | `in-progress` | 사용자 결정: channel-separated normalized infinity gates; four relative thresholds=`1e-2`; zero-scale 미결정 | `needs-requirements` | 같은 Requirement Agent가 free-DOF channel/same-trial scale/fresh-correction identity를 반영하고 zero-scale만 다음 질문으로 분리 | +| 2026-08-18 | Requirements OQ-021 nonzero-scale revision | `needs-rework` | revised `requirements.md`; 72/72 traceability, four `1e-2` channels, same-trial/fresh-solve scale, logical-AND/stable-order 및 sole pending-next 검증 | `needs-user-decision` | OQ-021 zero-denominator policy와 필요한 absolute thresholds를 사용자에게 질문 | +| 2026-08-18 | Requirements OQ-021 zero-scale policy partial decision | `in-progress` | 사용자 결정: channel-specific absolute fallback; exact four channel thresholds 미제공 | `needs-requirements` | 같은 Requirement Agent가 policy만 반영하고 four exact values/unit dimensions를 sole pending-next로 유지 | +| 2026-08-18 | Requirements OQ-021 zero-scale partial revision | `needs-rework` | revised `requirements.md`; 72/72 traceability, own-channel fallback, common floor/tolerance reuse absence와 four value/dimension request 검증 | `needs-user-decision` | force, force·length, length, dimensionless-rotation exact thresholds 네 값을 사용자에게 요청 | +| 2026-08-18 | Requirements OQ-021 final thresholds | `in-progress` | 사용자 결정: each zero-scale threshold numeric literal=`1e-3` with distinct model-consistent dimensions | `needs-requirements` | 같은 Requirement Agent가 OQ-021을 닫고 exact values/dimensions/pass rule/unit semantics/stale text를 전 구간 정렬 | +| 2026-08-18 | Requirements OQ-021 final revision | `needs-rework` | revised `requirements.md`; 72/72 traceability, OQ-021 closed/OQ-008 sole pending-next, four typed `1e-3`, nonzero `1e-2`, unit/fallback exclusion 검증 | `needs-user-decision` | OQ-008 line-search 지원 범위를 사용자에게 질문 | +| 2026-08-18 | Requirements OQ-008 | `in-progress` | 사용자 결정: option 1 `No line search` | `needs-requirements` | 같은 Requirement Agent가 full-correction direct application과 line-search/damping/merit/reduction/fallback exact absence를 반영하고 max iteration을 OQ-022로 분리 | +| 2026-08-19 | Requirements OQ-008 revision | `needs-rework` | user decision date 2026-08-18 유지; revised `requirements.md`; 72/72, OQ-008 closed/OQ-022 sole pending-next, full-correction identity와 line-search lifecycle exact absence 검증 | `needs-user-decision` | OQ-022 maximum Newton iteration count를 사용자에게 질문 | +| 2026-08-19 | Requirements OQ-022 | `in-progress` | 사용자 결정: attempted increment당 fixed maximum Newton iterations=`100` | `needs-requirements` | 같은 Requirement Agent가 iteration `1..100`, pass-at-100, fail-after-100 및 post-exhaustion exact absence를 반영 | +| 2026-08-19 | Requirements OQ-022 revision | `needs-rework` | revised `requirements.md`; 72/72, OQ-022 closed/OQ-010 sole pending-next, pass-at-99/100, fail-after-100와 post-event absence 검증 | `needs-user-decision` | OQ-010 finite-rotation/director state representation을 사용자에게 질문 | +| 2026-08-19 | Requirements OQ-010 | `in-progress` | 사용자 결정: `Incremental rotation vector + committed triad` | `needs-requirements` | 같은 Requirement Agent가 external DOF/incremental correction/committed-trial triad/multiplicative update/rollback과 downstream map gaps를 반영 | +| 2026-08-19 | Requirements OQ-010 revision | `needs-rework` | revised `requirements.md`; 75/75, OQ-010 closed/OQ-012 sole pending-next, triad/director invariants, exact rollback과 unresolved exact-map gaps 검증 | `needs-user-decision` | OQ-012 authoritative HDF5 accepted-frame/iteration-history 범위를 사용자에게 질문 | +| 2026-08-20 | Requirements OQ-012 | `in-progress` | user decision date 2026-08-19 유지: every committed increment frame, no trial history | `needs-requirements` | 같은 Requirement Agent가 accepted-commit↔frame 1:1/order/factor1 및 trial/failed/partial-final absence를 반영 | +| 2026-08-20 | Requirements OQ-012 revision | `needs-rework` | revised `requirements.md`; 75/75, OQ-012 closed/OQ-011 sole pending-next, accepted-frame bijection/order/factor1, absence/preservation와 factor0/schema gap 분리 검증 | `needs-user-decision` | OQ-011 runtime Newton diagnostic granularity를 사용자에게 질문 | +| 2026-08-21 | Requirements OQ-011 granularity/content | `in-progress` | 사용자 결정: every entered iteration exactly one structured runtime summary | `needs-requirements` | 같은 Requirement Agent가 complete/early-failure content, nonfabrication/order/runtime-only absence를 반영하고 transport/exit mapping을 분리 | +| 2026-08-21 | Requirements OQ-011 granularity revision | `needs-rework` | revised `requirements.md`; 77/77, OQ-011 closed/OQ-025 sole pending-next, completed/early-failure/exhaustion cardinality, nonfabrication와 HDF5/sidecar/reference absence 검증 | `needs-user-decision` | OQ-025 runtime-summary serialization format을 사용자에게 질문 | +| 2026-08-21 | Requirements OQ-025 | `in-progress` | 사용자 결정: `JSON Lines runtime records` | `needs-requirements` | 같은 Requirement Agent가 summary↔JSON-object↔line cardinality, finite/parseable/nonaggregation과 runtime-only absence를 반영하고 exact schema/transport/exit gaps를 분리 | +| 2026-08-21 | Requirements OQ-025 revision | `needs-rework` | revised `requirements.md`; 79/79, OQ-025 closed/OQ-026 sole pending-next, strict JSON Lines cardinality/finite/nonaggregation/order 및 projection absence 검증 | `needs-user-decision` | OQ-026 destination/buffering/failed-run delivery lifecycle을 사용자에게 질문 | +| 2026-08-21 | Requirements OQ-026 | `in-progress` | 사용자 결정: stderr record별 immediate emit+flush | `needs-requirements` | 같은 Requirement Agent가 flush-before-next/return, controlled failure delivery, stable/no-interleaving/no-bulk/no-stdout/projection absence를 반영 | +| 2026-08-21 | Requirements OQ-026 revision | `needs-rework` | revised `requirements.md`; 81/81, OQ-026 closed/OQ-028 sole pending-next, stderr emit/flush cardinality/order/delivery와 prohibited path absence 검증 | `needs-user-decision` | OQ-028 unavailable-field JSON schema를 사용자에게 질문 | +| 2026-08-21 | Requirements OQ-028 | `in-progress` | 사용자 결정: field omission + explicit not-evaluated identity list; low-risk defaults may auto-apply | `needs-requirements` | 같은 Requirement Agent가 omission/list nonfabrication을 반영하고 next item risk classification을 반환 | +| 2026-08-21 | Requirements OQ-028 revision | `needs-rework` | revised `requirements.md`; 82/82, OQ-028 closed/OQ-029 sole pending-next, omission-list bijection/reason/nonfabrication 검증; OQ-029 substantive 분류 | `needs-user-decision` | OQ-029 stderr write/flush failure policy를 사용자에게 질문 | +| 2026-08-21 | Requirements JSON policy scope reversal | `in-progress` | 사용자 요청: JSON 정책 철회, simple plain-text analysis log; destination은 substantive ambiguity | `needs-requirements` | 같은 Requirement Agent가 JSON-specific decisions/requirements를 retire하고 OQ-011을 보존한 뒤 stderr text 대 `.txt` file direct confirmation을 반환 | +| 2026-08-21 | Requirements JSON policy retirement rework | `needs-rework` | revised `requirements.md`; 82→77/77, retired NSNR-078..082, superseded/retired OQ-025..032, current JSON shall/Matrix 0, OQ-011 보존 검증 | `needs-user-decision` | OQ-033 stderr text 대 actual `.txt` file을 direct confirmation | +| 2026-08-21 | Requirements OQ-033 ambiguous response | `needs-rework` | 사용자 원문 verbatim evidence, OQ-033 `pending-clarification`/sole pending-next, 77/77 exact traceability와 금지범위 변경 0건 확인 | `needs-user-decision` | solver-only stderr와 external one-file redirect 의미를 direct yes/no로 확인 | +| 2026-08-21 | Requirements OQ-033 solver-managed file partial decision | `needs-rework` | Solver-managed single `.txt`, external redirect superseded, OQ-033 `pending-clarification`/sole pending-next, 77/77 exact traceability와 금지범위 변경 0건 확인 | `needs-user-decision` | same iteration summary의 file-only 대 file+stderr duplication을 direct confirmation | +| 2026-08-21 | Requirements OQ-033 file-only/no-duplication approval | `needs-rework` | OQ-033 closed; stderr duplicate 0; OQ-035 `analysis.log` sibling unapproved sole pending-next; repository evidence; 77/77 exact traceability와 금지범위 변경 0건 | `needs-user-decision` | OQ-035 filename/location direct confirmation | +| 2026-08-21 | Requirements input-stem output naming scope clarification | `needs-rework` | Exact proposal를 `proposed/pending-scope`로 기록, current shall/Matrix hit 0, OQ-035 sole pending-next, 77/77 exact traceability와 금지범위 변경 0건 | `needs-user-decision` | nonlinear-static-only 대 repository-wide scope direct confirmation | +| 2026-08-21 | Requirements repository-wide output scope approval | `in-progress` | 사용자 승인: all analyses input-directory stem outputs, remove `--output`; current one-input/explicit-output CLI/tests/ARCHITECTURE/ADR conflict read-only audit | `needs-requirements` | cross-procedure requirements와 global-doc handoff를 기록하고 removed-option compatibility를 sole pending-next로 분리 | +| 2026-08-21 | Requirements repository-wide output revision return | `needs-rework` | 77→80/80, NSNR-083..085, OQ-035 closed/OQ-038 sole pending-next, retired-ID reuse 0; NSNR-085 failure-atomicity scope ambiguity 발견 | `needs-requirements` | same Requirement Agent wording-only correction 후 evidence 재검증 | +| 2026-08-21 | Requirements failure-atomicity boundary correction | `needs-rework` | NSNR-085 legacy HDF5 preservation only; new result/log lifecycle OQ-037; 80/80 exact traceability; OQ-038 sole pending-next; forbidden changes 0 | `needs-user-decision` | OQ-038 strict removal/no-alias direct confirmation | +| 2026-08-22 | Requirements OQ-038 strict removal approval | `needs-rework` | OQ-038 closed; exact failure stage/code/diagnostic/output absence; OQ-036 unapproved sole pending-next; 80/80 exact traceability와 forbidden changes 0 | `needs-user-decision` | OQ-036 asymmetric lifecycle direct confirmation | +| 2026-08-22 | Requirements OQ-036 independent lifecycle approval | `needs-rework` | OQ-036 closed; approved log/HDF5 lifecycle and zero pair atomicity; OQ-037 unapproved sole pending-next; 80/80 exact traceability와 forbidden changes 0 | `needs-user-decision` | OQ-037 grouped log-I/O fail-closed direct confirmation | +| 2026-08-22 | Requirements OQ-037 grouped fail-closed approval | `needs-rework` | OQ-037 closed; NSNR-086 operation-stage/preservation/prohibited-event record; 81/81 exact traceability와 forbidden changes 0 | `needs-requirements` | OQ-034 low-risk auto-default revision | +| 2026-08-22 | Requirements OQ-037 revision evidence | `needs-rework` | OQ-037 closed, NSNR-086 added, 81/81 exact traceability, OQ-034 low-risk/OQ-039 first substantive classification | `needs-requirements` | OQ-034 auto-default bounded revision | +| 2026-08-22 | Requirements OQ-034 auto-default revision | `needs-rework` | OQ-034 closed, NSNR-087 added, 82/82 exact traceability, content/authority scope unchanged, OQ-039 sole pending-next | `needs-user-decision` | OQ-039 stem/path identity option selection | +| 2026-08-22 | Requirements OQ-039 lexical identity approval | `in-progress` | 사용자 option 1 approval; concurrency/locking remains substantive | `needs-requirements` | OQ-039 close, open-item audit, same-output concurrency question framing | +| 2026-08-22 | Requirements compact-pruning proposal | `needs-rework` | Read-only 24/24 proposal; 360–390 claim과 section sum 불일치, asymmetric output lifecycle mapping 보강 필요; file edits 0 | `needs-requirements` | Same Requirement Agent read-only correction | +| 2026-08-22 | Requirements compact-pruning corrected design | `needs-rework` | Exact 363-line budget, 24 canonical records/24 Matrix, approved semantic-loss 0, asymmetric log/HDF5 lifecycle explicit, Stage-1 remaining questions 0; baseline unchanged 2,909/83/83/40 | `needs-user-decision` | Compact sectioned-design 한 번의 명시적 사용자 승인 | +| 2026-08-22 | Requirements compact rewrite approval | `in-progress` | User explicitly approved 24-record/363-line-target design and permanent essential-decision-only Requirement Agent discipline | `needs-requirements` | Same Requirement Agent compact rewrite and self-audit | +| 2026-08-22 | Requirements compact rewrite return | `needs-rework` | 395 lines, exact 24↔24, no OQ/trivia/questions; Coordinator found NSNR-083 retained exit 2/pre-output but omitted approved pre-input/pre-Analysis precedence and no-alias/deprecation | `needs-requirements` | Same Requirement Agent NSNR-083 wording-only correction | +| 2026-08-22 | Requirements NSNR-083 correction return | `needs-rework` | 395 lines, exact 24↔24, NSNR-083 summary/record/Matrix preserve pre-input/pre-Analysis/pre-result-log exit 2 and no alias/deprecation; duplicate/missing/orphan/questions/placeholders/forbidden changes 0 | `needs-user-decision` | Present compact Stage-1 artifact for explicit user approval | +| 2026-08-23 | Requirements explicit user approval | `passed` | User explicitly approved `requirements.md`; owner and Coordinator evidence already passed | `research-in-progress` | Dispatch Research Agent for Stage 2 evidence | +| 2026-08-23 | Research Agent return and Coordinator audit | `needs-rework` | `research.md` owner pass; Coordinator verified 10 sections, S1–S17, 12 complete benchmark candidates, 11 requirement IDs, 14 unique open issues, local evidence existence, nonlinear stored reference hits 0 and forbidden changes 0 | `needs-user-decision` | Present Stage-2 artifact for explicit user approval | +| 2026-08-23 | Research explicit user approval | `passed` | User explicitly approved `research.md`; Research Agent and Coordinator evidence already passed; approved artifact SHA-256 `C920A6B02381230D1DB419D73FE767D611B36720D27D6410507BA88C3CA28EEE` | `needs-formulation` | Dispatch Formulation Agent for bounded Stage 3 evidence | +| 2026-08-23 | Formulation dispatch attempt 1 | `in-progress` | Approved Stage-1/2 baselines and project contracts audited; bounded package requires O-ROT/O-MAP/O-DRILL/O-MOM/O-BC closure without downstream contract changes | `needs-formulation` | Await Formulation Agent return and independently audit Stage-3 evidence | + +- current_dispatch: `stage-3-formulation-attempt-1` +- current_workflow_state: `needs-formulation` +- next_gate_requires_user_approval: `false` (owner evidence audit 선행) + +## 5. Risk, Blocker, and User-Decision Register + +| id | type | description | owner | status | +| --- | --- | --- | --- | --- | +| RISK-001 | architecture | 기존 `LinearStaticAnalysis` private lifecycle은 단일 factorization/substitution과 final frame만 소유하므로 nonlinear increment/iteration/state commit을 삽입하면 ADR 경계를 위반한다. | `coordinator-agent` routing | open | +| RISK-002 | scope | `Newton–Raphson`은 solution algorithm이고 geometric/material/contact nonlinearity 범위를 단독으로 결정하지 않는다. | `requirement-agent` | mitigated by DECISION-001 | +| RISK-003 | contract | 현재 `Element`는 displacement-dependent residual/consistent tangent/trial state 계약이 없고 `AnalysisState`는 nonlinear history를 소유하지 않는다. | downstream formulation/architecture gates | open | +| RISK-004 | input | 현재 `NLGEOM=YES`는 `unsupported-nonlinear-geometry`로 거부되고 `*STATIC` 네 값은 provenance로만 보존된다. | downstream requirements/I/O gates | open | +| RISK-005 | verification | exact nonlinear reference artifacts와 path-dependent blocking quantities가 아직 지정되지 않았다. | downstream numerical-review gate | open | +| DECISION-001 | user decision | 첫 release는 materially linear + geometrically nonlinear MITC4로 고정한다. Material-only와 combined material/geometric nonlinearity는 이 release 범위 밖이다. | user via Coordinator | closed | +| DECISION-002 | user decision | First-release geometric-nonlinear MITC4 kinematic framework는 initial configuration 기준 `Total Lagrangian`으로 고정한다. Updated Lagrangian과 corotational 의미는 이 release 범위 밖이다. | user via Coordinator | closed | +| DECISION-003 | user decision | Newton variant는 `Full Newton–Raphson`으로 고정한다. 매 iteration의 current trial/candidate state에서 residual과 algorithmically consistent tangent를 재평가하고, 그 tangent로 새 factorization/solve를 수행한다. Modified Newton과 adaptive refresh는 out-of-scope다. | user via Coordinator | closed | +| DECISION-004 | user decision | First-release nonlinear increment control은 하나의 scalar load coordinate/load factor로 approved load/BC path를 진행하는 `Load-factor control`로 고정한다. Controlled-displacement와 arc-length/path-following control은 out-of-scope다. | user via Coordinator | closed | +| DECISION-005 | user decision | 모든 approved `*CLOAD`와 nonzero prescribed `*BOUNDARY` target은 같은 dimensionless scalar load factor로 step-start 값에서 target까지 비례 진행한다. Fixed step-start BC와 independent/non-proportional amplitude/path는 out-of-scope다. | user via Coordinator | closed | +| DECISION-006 | user decision | First-release는 approved fixed load-factor increment size를 반복하고 factor 1에 정확히 도달하도록 마지막 increment만 작게 조정하는 `Fixed-size stepping`으로 고정한다. Automatic growth, cutback/retry와 explicit schedule은 out-of-scope며 attempted increment failure는 재시도 없이 analysis failure다. | user via Coordinator | closed | +| DECISION-007 | user decision | Nonlinear four-value `*STATIC`은 first positive value만 fixed load-factor increment로 사용하고 second/period는 exact supported endpoint `1`을 요구하며 positive minimum/maximum은 입력 호환성을 위해 수용하지만 runtime stepping에는 사용하지 않는 `First-value driven` mapping으로 고정한다. Strict tuple과 single-value form은 out-of-scope다. | user via Coordinator | closed | +| DECISION-008 | user decision | First-release approved `*CLOAD` force/moment component directions는 initial/current deformation과 무관하게 fixed global frame에 유지되고 common scalar factor로 magnitude만 비례 진행하는 dead-load semantics로 고정한다. Follower nodal loads, selectable dual semantics, external-load geometric tangent/follower work는 out-of-scope다. | user via Coordinator | closed | +| DECISION-009 | user decision | Nonzero prescribed `*BOUNDARY` input value는 factor 1의 absolute global-DOF `Total step target`이며 step-start committed value에서 target까지 common scalar factor로 보간한다. Incremental delta와 selectable dual semantics는 out-of-scope다. | user via Coordinator | closed | +| DECISION-010 | user decision | First release는 입력당 exactly one supported geometrically nonlinear static step만 허용하고 no-prior-history baseline에서 factor 0→1을 수행한다. Multiple nonlinear steps, mixed linear/nonlinear steps, cross-step state/load/BC propagation과 procedure transition은 out-of-scope/fail-closed다. | user via Coordinator | closed | +| DECISION-011 | user decision | First-release increment acceptance는 free-DOF equilibrium residual과 Newton correction의 두 mandatory quantity가 각각 승인 gate를 모두 통과해야 한다. Energy convergence는 diagnostic/mandatory가 아닌 out-of-scope다. Norm, normalization과 tolerance는 별도 결정으로 남긴다. | user via Coordinator | closed | +| DECISION-012 | user decision | Four channel-separated infinity gates의 nonzero-scale relative threshold는 각각 `1e-2`다. Zero denominator에는 own-channel absolute fallback을 적용하며 네 numeric literal은 모두 `1e-3`: force residual은 model-consistent force, moment residual은 force·length, translational correction은 length, rotational correction은 later-approved convention의 dimensionless rotation parameter다. `.inp` 단위 추론/변환은 하지 않는다. | user via Coordinator | closed | +| DECISION-013 | user decision | First release는 `No line search`다. 각 successful fresh tangent correction solve의 full correction을 damping/backtracking/trial-step reduction 없이 next candidate에 그대로 적용하며 merit/acceptance/reduction loop, selectable input과 fallback은 out-of-scope/fail-closed다. | user via Coordinator | closed | +| DECISION-014 | user decision | Attempted increment당 maximum Newton iteration count는 product-fixed `100`이다. Entered iteration은 `1..100`; iteration 100 gate pass는 accept 가능하고 fail 시 iteration 101/candidate/retry/cutback 없이 immediate failure 및 prior committed state/result preservation을 적용한다. | user via Coordinator | closed | +| DECISION-015 | user decision | MITC4 Newton solve는 dimensionless incremental rotation-vector correction을 만들고 authoritative rotational state는 orthonormal right-handed committed triad `Q`이며 director는 third axis다. Separate trial triad를 사용하고 large rotation은 multiplicative composition으로 갱신한다. Exact map/side/frame/parameterization/re-orthonormalization/drilling/derivatives는 downstream gap이다. | user via Coordinator | closed | +| DECISION-016 | user decision | Successful analysis의 authoritative `results.h5`는 each committed nonlinear increment마다 exactly one accepted frame을 stable accepted-factor order로 저장하고 factor-1 frame을 포함한다. Trial/failed/duplicate/missing/partial-final history는 없으며 pre-existing valid final을 exact 보존한다. Exact schema와 factor-0 frame 여부는 downstream gap이다. | user via Coordinator | closed | +| DECISION-017 | user decision | Every entered Newton iteration은 exactly one deterministic structured runtime summary를 낸다. Complete gate는 four-channel identities/norms/branch/threshold/pass/combined transition을 포함하고 early failure는 last-completed/failing stage와 later fields absent/not-evaluated를 기록한다. 이는 diagnostic-only이며 HDF5/sidecar/authoritative/reference quantity가 아니다. Transport/exit mapping은 별도 미결정이다. | user via Coordinator | closed | +| DECISION-018 | superseded user decision | JSON Lines serialization family 결정은 DECISION-023 scope reversal로 current contract에서 retire되며 historical evidence로만 남는다. | user via Coordinator | closed | +| DECISION-019 | superseded user decision | JSON stderr exactly-once emit/flush lifecycle 결정은 DECISION-023 scope reversal로 current contract에서 retire되며 historical evidence로만 남는다. | user via Coordinator | closed | +| DECISION-020 | superseded user decision | JSON field-omission/not-evaluated-list 결정은 DECISION-023 scope reversal로 current contract에서 retire되며 historical evidence로만 남는다. | user via Coordinator | closed | +| DECISION-021 | user operating policy | 물리 결과·수치 거동·public compatibility에 실질 영향 없는 serialization notation/key ordering/diagnostic formatting 등 low-risk 기본 결정은 recommended option을 자동 적용한다. Formulation/Newton/state/tolerance/load-BC/input/failure-rollback/HDF5 authoritative/public compatibility/reference acceptance는 계속 한 번에 하나씩 인터뷰한다. | user via Coordinator | closed | +| DECISION-022 | retired pending decision | JSON stderr write/flush failure policy는 DECISION-023 scope reversal로 선택 없이 retire되었다. | user via Coordinator | closed | +| DECISION-023 | user scope reversal | JSON-specific runtime log decisions와 파생 contracts를 철회하고 serialization-independent OQ-011 granularity를 보존한 simple plain-text analysis log로 재설계한다. Destination은 stderr text 대 actual `.txt` file의 substantive user decision으로 남긴다. | user via Coordinator | closed | +| DECISION-024 | user decision | Solver directly creates exactly one separate plain-text analysis-log file. Per-iteration summaries are file-only; stderr contains log open/write/close fatal diagnostic and final analysis failure summary only, with exact zero per-iteration duplication. External redirect and file+stderr duplication are excluded. Filename/location, overwrite and failure atomicity remain separate questions. | user via Coordinator | closed | +| DECISION-025 | user decision | Repository-wide architectural direction approved: all existing/future analyses use input-directory `.inp -> _results.h5` and `_log.txt`, and `--output` is removed. This requires later approved sectioned-design changes to ARCHITECTURE/ADR and cross-procedure regression evidence; no implementation/global-doc change is claimed now. | user via Coordinator | closed | +| DECISION-026 | user decision | Every invocation containing `--output`, including the formerly valid explicit path form, fails before input parsing/Analysis construction/result-log creation with exact exit 2 and one ordered `cli-usage` stderr diagnostic. No compatibility alias or deprecation window. | user via Coordinator | closed | +| DECISION-027 | user decision | Independent asymmetric lifecycle: current-run log replaces/truncates old log at invocation start and persists on success/failure; HDF5 uses sibling candidate and replaces final only after success, preserving prior valid final on failure; no cross-file pair atomicity. | user via Coordinator | closed | +| DECISION-028 | user decision | Log-I/O grouped fail-closed policy: pre-analysis abort on create/open/truncate failure; immediate abort on write/flush; close failure blocks result commit; best-effort one fatal stderr diagnostic attempt, prior HDF5 and retained log prefix preservation, no retry/fallback/continue/result commit. | user via Coordinator | closed | +| DECISION-029 | coordinator auto-default | OQ-034 low-risk plain-text representation/ordering: UTF-8 no BOM, one physical tab-separated `label=value` line per entered iteration, fixed semantic field/channel order, explicit `not-evaluated(reason)`, locale-independent finite round-trip numerics, embedded control/backslash escaping. No physics/numerics/path/state/authority change. | Coordinator under DECISION-021 | closed | +| DECISION-030 | user decision | OQ-039 user-addressed lexical identity: resolve relative input against invocation CWD, lexically normalize `.`/`..`, do not resolve symlink/junction targets, accept final `.inp` case-insensitively, remove only the last extension and preserve preceding dots/basename case; output beside normalized user-addressed path. | user via Coordinator | closed | +| DECISION-031 | superseded proposal | Same-derived-output concurrent invocation ownership의 fine-grained OQ-040 interview는 사용자 process correction으로 중단했다. 승인된 정책은 없으며 필요한 convention은 I/O/Planning owner가 repository evidence로 정한다. | user via Coordinator | closed | +| DECISION-032 | user process decision | `requirements.md`를 핵심 Stage-1 계약으로 압축하고 OQ chronology, diagnostic/path/concurrency trivia와 반복 handoff를 제거한다. Minor details는 downstream specialist convention/evidence로 정하며 approved scope/physics/tolerance/public compatibility를 바꿀 때만 사용자 결정을 다시 요청한다. | user via Coordinator | closed | +| DECISION-033 | design approval | Target 363 lines, 24 canonical requirements와 24-row Matrix, approved semantic-loss 0의 compact rewrite design. | user via Coordinator | closed | +| DECISION-034 | user process decision | Requirement Agent는 approved physics/scope/tolerance/authoritative-output/public compatibility를 바꾸는 essential decision만 사용자에게 묻고, specialist detail은 owning downstream stage가 repository evidence와 conventional FEM practice로 정한다. Equivalence claim은 금지한다. | user via Coordinator; `.codex/agents/requirement-agent.toml` | closed | + +## 6. Rework-Loop Control and Stop Condition + +- normalized_failure_attempts: `requirements-next-question-routing-mismatch`: 1; `requirements-output-failure-atomicity-scope-ambiguity`: 1; `requirements-compact-public-contract-omission`: 1 +- automatic_rework_limit: 동일 normalized failure classification `2`회 +- correction_agent_policy: 명확한 implementation failure는 먼저 `implementation-agent`에 반환하고, 반복되거나 원인이 불명확할 때만 `correction-agent`를 dispatch한다. +- stop_condition: 동일 classification이 두 번이면 자동 rework를 중단하고 workflow를 `needs-user-decision` 또는 `blocked`로 전환한다. + +## 7. Final Workflow Closure + +- closure_status: `not-eligible` +- required_evidence: `docs/nonlinear-static-newton-raphson/release.md`의 `ready-for-release` recommendation +- closure_record: 없음 + +## 8. No-Change Assertion + +- source_code: 변경 없음 +- tests: 변경 없음 +- CMake: 변경 없음 +- reference_artifacts: 생성·수정·rename 없음 +- tolerance_policies: 변경 없음 +- phase_files: 생성 없음 +- Harness: 실행하지 않음 +- feature_documents: `coordination.md`, `requirements.md`, `research.md`만 생성됨 diff --git a/docs/nonlinear-static-newton-raphson/requirements.md b/docs/nonlinear-static-newton-raphson/requirements.md new file mode 100644 index 0000000..74f2fd3 --- /dev/null +++ b/docs/nonlinear-static-newton-raphson/requirements.md @@ -0,0 +1,397 @@ +# Nonlinear Static Newton–Raphson 요구조건 + +## 1. Metadata +- feature_id: `nonlinear-static-newton-raphson` +- title: `Nonlinear Static Analysis Using Newton–Raphson` +- status: `approved` +- owner_agent: `requirement-agent` +- date: `2026-08-22` +- approved_by: user +- approval_date: `2026-08-23` +- authoritative_scope: materially linear, geometrically nonlinear `S4/S4R -> FESA-MITC4` +- independence: FESA는 독립 solver이며 Abaqus 또는 Midas의 내부 알고리즘 동등성을 주장하지 않는다. +- unit_policy: `.inp` 단위계를 추론하거나 변환하지 않고 사용자가 일관되게 제공한 단위계를 보존한다. + +Parent needs: `NEED-NSNR-001` nonlinear procedure, `NEED-NSNR-002` physics/numerical correctness, +`NEED-NSNR-003` state/output integrity, `NEED-NSNR-004` independent verification. + +## 2. Purpose and Expected Behavior +FESA는 하나의 지원 nonlinear static step을 scalar load factor로 증가시키며 Full Newton–Raphson으로 각 증분의 평형을 구한다. 수렴한 증분만 atomically commit하고 authoritative accepted result로 기록한다. 기존 linear-static physics와 결과 의미는 보존하되 repository-wide derived output naming은 이 기능과 함께 적용할 승인 방향이다. + +## 3. In Scope +- Abaqus source `S4`, `S4R`의 FESA-MITC4 mapping과 homogeneous isotropic linear elasticity +- fixed-initial-reference Total Lagrangian geometric nonlinearity와 finite rotational state +- same-trial residual/algorithmically consistent tangent, fresh factorization/solve의 Full Newton +- fixed scalar load-factor increments, common proportional load/BC path, fixed-global dead `*CLOAD` +- factor-1 absolute prescribed `*BOUNDARY` targets와 four-value nonlinear `*STATIC` +- four-channel residual/correction convergence, maximum 100 iterations, no line search +- separate trial state, atomic commit/rollback, accepted-frame HDF5와 per-iteration text log +- deterministic assembly, iteration, frame, result, diagnostic order와 stored-reference verification + +## 4. Out Of Scope +- material nonlinearity, nonlinear material history, combined material/geometric nonlinearity +- Updated Lagrangian, corotational procedure, multiple or mixed nonlinear steps, cross-step propagation +- follower load, non-proportional path, controlled-displacement, arc-length/path-following +- modified/adaptive Newton, tangent reuse, line search, damping, automatic growth/cutback/retry +- energy/work convergence, trial-state HDF5 history, direct reference-solver execution +- Abaqus/Midas formulation, stabilization, state update 또는 결과 절차의 내부 동등성 + +## 5. Analysis Definition +| item | approved meaning | +| --- | --- | +| analysis | exactly one nonlinear static step from a no-prior-history baseline | +| elements | `S4`, `S4R` source types map to materially linear FESA-MITC4 | +| DOFs | global `[UX, UY, UZ, URX, URY, URZ]`; rotational correction is dimensionless | +| kinematics | Total Lagrangian relative to one fixed initial configuration | +| rotation state | committed orthonormal right-handed triad `Q`; director is its third axis; separate trial triad/director; multiplicative finite-rotation update | +| material | homogeneous isotropic linear elasticity; no nonlinear material state | +| control | one dimensionless scalar load factor with fixed increments and final shortening to factor 1 | +| Newton | same-trial residual and consistent tangent, fresh factorization and correction solve every iteration | +| convergence | translational-force residual, rotational-moment residual, translational correction, rotational correction; all four must pass with `<=` | +| loads/BCs | fixed-global dead `*CLOAD`; factor-1 absolute `*BOUNDARY` targets on one proportional path | +| state | candidate/trial remains separate; complete converged increment commits atomically | +| coordinates/units | nodal values are global unless an approved element-local quantity states otherwise; user-consistent units without inference/conversion | + +Exact Total Lagrangian shell equations, strain/stress measures, rotation map details, drilling treatment and consistent derivatives belong to Research/Formulation and Numerical Review without changing this approved scope. + +## 6. Input Requirements +- Nonlinear execution requires exactly one supported nonlinear static source step and one semantic step. +- Supported first-release meanings are limited to the approved MITC4 material/section, nonlinear `*STATIC`, `*CLOAD`, and `*BOUNDARY` subset. +- Nonlinear `*STATIC` has four positive finite values: first is the fixed increment, second represents endpoint 1 exactly, and third/fourth are accepted for compatibility but unused by stepping. +- Nonzero prescribed `*BOUNDARY` values are factor-1 absolute global-DOF targets; approved `*CLOAD` components are fixed-global dead forces or moments. +- Unsupported, ambiguous, missing, nonfinite, or out-of-scope meanings fail closed rather than falling back to linear or alternate nonlinear behavior. + +## 7. Output Requirements +- Successfully committed increments map one-to-one to authoritative accepted HDF5 frames in load-factor order and include the factor-1 frame; trial history is not authoritative output. +- `_results.h5` is completed as a sibling candidate and replaces the final only after success; failure preserves a prior valid final. +- `_log.txt` is replaced/truncated at invocation start and remains the current-run live audit after controlled success or failure. +- Every entered Newton iteration has one deterministic diagnostic-only text summary; exact representation and low-level I/O mechanics belong to I/O Definition. +- Every analysis procedure uses input-directory `_results.h5` and `_log.txt`; every invocation containing literal `--output` treats it as unrecognized and fails with exit code 2 before input parsing, Analysis, result-candidate, log, or output creation, with no compatibility alias or deprecation window. Result and log lifecycles are independent, not a cross-file all-or-nothing commit. +- Exact HDF5 paths/shapes, factor-0 projection, triad projection, compression/chunking and path/collision conventions belong to I/O Definition. + +## 8. Requirement Records +```yaml +- id: FESA-REQ-NSNR-001 + statement: "The FESA solver shall execute nonlinear static analysis through a separate procedure only when exactly one supported nonlinear source step maps to exactly one semantic step from a no-prior-history baseline." + category: functional + rationale: "Procedure cardinality and lifecycle must be unambiguous." + source: user + priority: must + verification_method: test + acceptance_criteria: "One valid step selects one nonlinear procedure; zero, multiple, mixed, or ambiguous nonlinear steps fail before an attempted nonlinear increment, while unselected approved linear analysis retains its established behavior." + tolerance: "Exact source/semantic cardinality and procedure identity." + trace_to: {parent_need: "NEED-NSNR-001", downstream_agents: ["I/O Definition Agent", "Implementation Planning Agent"]} + status: approved +- id: FESA-REQ-NSNR-003 + statement: "The FESA solver shall support only materially linear, geometrically nonlinear FESA-MITC4 for source types S4 and S4R in the first release." + category: physics + rationale: "The approved release is geometric-only and must not create nonlinear material state." + source: user + priority: must + verification_method: test + acceptance_criteria: "Supported S4/S4R cases use homogeneous isotropic linear elasticity and MITC4; material-nonlinear or combined-nonlinearity input fails closed." + tolerance: "Exact supported element/material inventory." + trace_to: {parent_need: "NEED-NSNR-002", downstream_agents: ["Research Agent", "Formulation Agent", "Numerical Review Agent"]} + status: approved +- id: FESA-REQ-NSNR-041 + statement: "The FESA solver shall use Total Lagrangian kinematics relative to one fixed initial reference configuration." + category: physics + rationale: "The formulation reference must not change across increments." + source: user + priority: must + verification_method: analysis + acceptance_criteria: "Every increment and accepted state retains the same initial-reference identity; current geometry is only a derived observable and never re-bases the formulation." + tolerance: "Reference identity exact; numerical kinematic tolerances are owned by Numerical Review." + trace_to: {parent_need: "NEED-NSNR-002", downstream_agents: ["Research Agent", "Formulation Agent", "Numerical Review Agent"]} + status: approved +- id: FESA-REQ-NSNR-074 + statement: "The FESA solver shall retain global DOFs [UX, UY, UZ, URX, URY, URZ], use a dimensionless incremental rotation correction, and maintain separate trial and committed finite-rotation triad/director states." + category: physics + rationale: "Large rotations require an objective state distinct from failed candidates." + source: user + priority: must + verification_method: analysis + acceptance_criteria: "Committed Q is orthonormal and right-handed, its third axis is the director, candidate updates are multiplicative, successful commit transfers the complete state, and failure preserves the prior committed state." + tolerance: "State identity exact; Q invariants use Numerical Review-approved tolerances." + trace_to: {parent_need: "NEED-NSNR-002, NEED-NSNR-003", downstream_agents: ["Research Agent", "Formulation Agent", "Numerical Review Agent"]} + status: approved +- id: FESA-REQ-NSNR-006 + statement: "The FESA solver shall perform Full Newton iterations using the same current-trial residual and algorithmically consistent tangent, followed by a fresh tangent factorization and correction solve." + category: numerical + rationale: "Residual, tangent, factorization, and correction must describe one trial state." + source: user + priority: must + verification_method: test + acceptance_criteria: "Each entered iteration records one trial identity shared by residual and tangent, factorizes that tangent after evaluation, and solves its correction with that fresh factorization before convergence or update." + tolerance: "Trial/factorization identity and event order exact." + trace_to: {parent_need: "NEED-NSNR-002", downstream_agents: ["Formulation Agent", "Numerical Review Agent", "Implementation Planning Agent"]} + status: approved +- id: FESA-REQ-NSNR-007 + statement: "The FESA solver shall accept an increment only when its free-DOF equilibrium residual and same-iteration free-DOF Newton correction gates all pass." + category: numerical + rationale: "Equilibrium and update size are both required convergence evidence." + source: user + priority: must + verification_method: test + acceptance_criteria: "All four channel results are combined by logical AND; constrained DOFs are excluded from convergence and their full-equilibrium residual retains reaction meaning." + tolerance: "The four channel policies in NSNR-069 and NSNR-070 apply with inclusive <= comparisons." + trace_to: {parent_need: "NEED-NSNR-002", downstream_agents: ["Numerical Review Agent", "Implementation Planning Agent"]} + status: approved +- id: FESA-REQ-NSNR-069 + statement: "The FESA solver shall evaluate translational-force and rotational-moment free-residual convergence with channel-separated infinity-norm gates." + category: numerical + rationale: "Force and moment dimensions require separate scales." + source: user + priority: must + verification_method: test + acceptance_criteria: "For a nonzero matching-channel denominator max(||internal||inf, ||external||inf), the same-trial residual ratio passes iff <=1e-2; an exact-zero denominator instead passes iff its numerator is <=1e-3 model-consistent force or <=1e-3 model-consistent force-length, respectively." + tolerance: "Relative 1e-2 dimensionless; zero-scale absolute 1e-3 force and 1e-3 force-length." + trace_to: {parent_need: "NEED-NSNR-002", downstream_agents: ["Numerical Review Agent", "Implementation Planning Agent"]} + status: approved +- id: FESA-REQ-NSNR-070 + statement: "The FESA solver shall evaluate translational and rotational free-correction convergence with channel-separated infinity-norm gates." + category: numerical + rationale: "Translation and rotation corrections have different dimensions." + source: user + priority: must + verification_method: test + acceptance_criteria: "For a nonzero current-trial incremental-solution denominator relative to the step-start committed state, the fresh-correction ratio passes iff <=1e-2; an exact-zero denominator instead passes iff its numerator is <=1e-3 model-consistent length or <=1e-3 dimensionless rotation, respectively." + tolerance: "Relative 1e-2 dimensionless; zero-scale absolute 1e-3 length and 1e-3 dimensionless rotation." + trace_to: {parent_need: "NEED-NSNR-002", downstream_agents: ["Numerical Review Agent", "Implementation Planning Agent"]} + status: approved +- id: FESA-REQ-NSNR-008 + statement: "The FESA solver shall permit entered Newton iteration identities 1 through 100 and shall reject nonfinite required iteration data." + category: numerical + rationale: "The iteration limit and finite-data boundary must be deterministic." + source: user + priority: must + verification_method: test + acceptance_criteria: "A pass at iteration 100 may commit; otherwise iteration 100 ends in nonconvergence without iteration 101, and any nonfinite required residual, tangent, correction, state, load, or recovery value fails before acceptance." + tolerance: "Iteration identities and finite predicates exact." + trace_to: {parent_need: "NEED-NSNR-002, NEED-NSNR-003", downstream_agents: ["Numerical Review Agent", "Implementation Planning Agent"]} + status: approved +- id: FESA-REQ-NSNR-014 + statement: "The FESA solver shall apply each successful fresh Newton correction unchanged when another iteration is required and shall use no line search, damping, solver fallback, or energy/work convergence gate." + category: constraint + rationale: "The approved first release uses direct Full Newton updates only." + source: user + priority: must + verification_method: test + acceptance_criteria: "The next candidate uses the fresh solve output without scalar or component modification; convergence depends only on NSNR-069 and NSNR-070." + tolerance: "Correction/update identity exact." + trace_to: {parent_need: "NEED-NSNR-002", downstream_agents: ["Numerical Review Agent", "Implementation Planning Agent"]} + status: approved +- id: FESA-REQ-NSNR-046 + statement: "The FESA solver shall advance one scalar load factor by a fixed positive increment, shortening only the final increment to reach factor one without growth, cutback, or retry." + category: numerical + rationale: "Fixed stepping provides the approved deterministic load path." + source: user + priority: must + verification_method: test + acceptance_criteria: "The intended and accepted factor sequence starts at zero, never overshoots one, ends at the discrete factor-one identity on success, and analysis failure creates no replacement attempt." + tolerance: "Factor/order identity exact; endpoint arithmetic is fixed by Numerical Review before implementation." + trace_to: {parent_need: "NEED-NSNR-002", downstream_agents: ["Numerical Review Agent", "Implementation Planning Agent"]} + status: approved +- id: FESA-REQ-NSNR-048 + statement: "The FESA solver shall advance every approved CLOAD and nonzero prescribed BOUNDARY target on one common proportional scalar load-factor path." + category: physics + rationale: "Loads and prescribed values must share one path identity." + source: user + priority: must + verification_method: test + acceptance_criteria: "Factor zero reproduces step-start values, intermediate states use the same factor for all approved targets, and factor one reproduces every target." + tolerance: "Load-factor and target identity exact." + trace_to: {parent_need: "NEED-NSNR-002", downstream_agents: ["Formulation Agent", "Numerical Review Agent"]} + status: approved +- id: FESA-REQ-NSNR-018 + statement: "The FESA solver shall interpret approved CLOAD force and moment components as dead loads fixed in global directions while the common factor scales magnitude only." + category: physics + rationale: "Follower-load behavior would change equilibrium and tangent meaning." + source: user + priority: must + verification_method: test + acceptance_criteria: "Force and moment source DOF directions remain unchanged with deformation, moments retain force-length dimensions, and no follower external-load tangent is used." + tolerance: "Global component identity exact; values use the model-consistent unit system." + trace_to: {parent_need: "NEED-NSNR-002", downstream_agents: ["Formulation Agent", "Numerical Review Agent"]} + status: approved +- id: FESA-REQ-NSNR-063 + statement: "The FESA solver shall interpret each approved nonzero BOUNDARY value as a factor-one absolute global-DOF target interpolated from its step-start committed value." + category: physics + rationale: "Absolute prescribed values must not be confused with correction increments." + source: user + priority: must + verification_method: test + acceptance_criteria: "The prescribed current value follows the common factor, zero start/target remains zero, the constrained correction is distinct from that value, and failed candidates do not change the step-start value." + tolerance: "Prescribed path/source identity exact; values use model-consistent displacement or rotation units." + trace_to: {parent_need: "NEED-NSNR-002, NEED-NSNR-003", downstream_agents: ["Formulation Agent", "Numerical Review Agent"]} + status: approved +- id: FESA-REQ-NSNR-016 + statement: "The FESA solver shall map nonlinear STATIC four-value data with the first positive finite value as fixed increment, the second as endpoint one, and positive finite third and fourth values accepted but unused by stepping." + category: input + rationale: "The approved compatibility fields must not alter fixed stepping." + source: user + priority: must + verification_method: test + acceptance_criteria: "Valid four-value data records the first value for runtime use and identifies the third/fourth as unused; invalid arity, nonfinite/nonpositive required values, or period not representing one fails closed." + tolerance: "Parsed endpoint-one identity exact; warning representation is owned by I/O Definition." + trace_to: {parent_need: "NEED-NSNR-001", downstream_agents: ["I/O Definition Agent", "Implementation Planning Agent"]} + status: approved +- id: FESA-REQ-NSNR-011 + statement: "The FESA solver shall keep trial state separate and atomically commit a complete converged displacement, rotation/director, load-factor, frame, force, and recovery state while preserving the prior committed state on failure." + category: functional + rationale: "Partial nonlinear state commits would corrupt continuation and results." + source: user + priority: must + verification_method: test + acceptance_criteria: "Successful validation commits one coherent state identity; iteration, increment, recovery, or output failure leaves the prior committed state and authoritative final result unchanged." + tolerance: "State and commit identity exact." + trace_to: {parent_need: "NEED-NSNR-003", downstream_agents: ["Formulation Agent", "Numerical Review Agent", "Implementation Planning Agent"]} + status: approved +- id: FESA-REQ-NSNR-019 + statement: "The FESA solver shall preserve stable source identity and stable assembly order and shall derive free residual and constrained reaction from the complete assembled equilibrium at the same state." + category: physics + rationale: "Equilibrium evidence must remain traceable to source entities and DOFs." + source: docs + priority: must + verification_method: test + acceptance_criteria: "Input instance/label/component maps deterministically through assembly, state, diagnostic, result, and comparison; full residual at a trial or accepted state yields free-equilibrium evidence and constrained reactions." + tolerance: "Source/component identity and discrete order exact; equilibrium uses approved numerical tolerances." + trace_to: {parent_need: "NEED-NSNR-002, NEED-NSNR-004", downstream_agents: ["Formulation Agent", "Numerical Review Agent", "I/O Definition Agent"]} + status: approved +- id: FESA-REQ-NSNR-020 + statement: "The FESA solver shall fail closed on every input or model meaning outside the approved element, material, load, boundary, step, and solver scope." + category: input + rationale: "Unsupported nonlinear behavior must not become a warning-only or linear fallback." + source: docs + priority: must + verification_method: test + acceptance_criteria: "A negative inventory for each unsupported class rejects the model before nonlinear state or authoritative output is committed." + tolerance: "Exact supported/unsupported inventory." + trace_to: {parent_need: "NEED-NSNR-001", downstream_agents: ["I/O Definition Agent", "Implementation Planning Agent"]} + status: approved +- id: FESA-REQ-NSNR-021 + statement: "The FESA solver shall create authoritative accepted HDF5 frames one-to-one with committed increments, including factor one, using a sibling candidate that replaces the final only on success and preserves a prior valid final on failure." + category: output + rationale: "Authoritative results must contain accepted states only and remain failure-safe." + source: user + priority: must + verification_method: test + acceptance_criteria: "Committed increment and accepted-frame identities match in factor order, the successful result includes factor one, trial Newton history is absent, and controlled failure does not expose the candidate as final or damage a prior valid final." + tolerance: "Commit/frame identity exact; numerical quantities use their approved verification tolerances." + trace_to: {parent_need: "NEED-NSNR-003", downstream_agents: ["Numerical Review Agent", "I/O Definition Agent", "Implementation Planning Agent"]} + status: approved +- id: FESA-REQ-NSNR-024 + statement: "The FESA solver shall replace or truncate the single derived text log at invocation start, retain it as the current-run live audit on controlled success or failure, and produce one deterministic diagnostic-only summary for every entered Newton iteration." + category: output + rationale: "Iteration evidence is required without making trial states authoritative results." + source: user + priority: must + verification_method: test + acceptance_criteria: "Completed and early-failure iterations preserve their stable iteration/stage and convergence meaning in entered order; the log remains current-run diagnostic evidence and is not HDF5 trial history or reference data." + tolerance: "Summary cardinality and semantic identity exact; representation and low-level failure presentation are owned by I/O Definition." + trace_to: {parent_need: "NEED-NSNR-003", downstream_agents: ["I/O Definition Agent", "Implementation Planning Agent"]} + status: approved +- id: FESA-REQ-NSNR-083 + statement: "The FESA solver shall apply repository-wide input-directory names _results.h5 and _log.txt, treat every invocation containing literal --output as unrecognized and fail it with exit code 2 before input parsing, Analysis, result-candidate, log, or output creation without a compatibility alias or deprecation window, and use independent asymmetric result/log lifecycles without cross-file all-or-nothing commit." + category: output + rationale: "Public output identity and authority must be consistent across procedures." + source: user + priority: must + verification_method: test + acceptance_criteria: "Every existing and future procedure derives the two approved names beside its input and preserves linear-static numerical/HDF5 meaning under the migration; every argument form containing literal --output fails as unrecognized with exit code 2 before input parsing, Analysis, result-candidate, log, or output creation and has no accepted alias or deprecation form; log initialization does not commit HDF5 and HDF5 failure does not roll back the live log." + tolerance: "Names, exit code, lifecycle independence, and regression identity exact; path and ownership mechanics are downstream decisions." + trace_to: {parent_need: "NEED-NSNR-003", downstream_agents: ["I/O Definition Agent", "Implementation Planning Agent", "Numerical Review Agent"]} + status: approved +- id: FESA-REQ-NSNR-026 + statement: "The FESA solver shall produce deterministic increment, iteration, assembly/reduction, accepted-frame, result-row, and diagnostic ordering for the same input and approved runtime configuration." + category: constraint + rationale: "Reproducible numerical and reference evidence requires stable discrete ordering." + source: docs + priority: must + verification_method: test + acceptance_criteria: "Repeated runs and approved thread configurations preserve the same intended/attempted/accepted factor identities, Newton event sequence, sparse/reduction structure, frame order, result identities, and log order." + tolerance: "Discrete structure/order exact; floating equality policy is set by Numerical Review from repository conventions." + trace_to: {parent_need: "NEED-NSNR-003, NEED-NSNR-004", downstream_agents: ["Numerical Review Agent", "Implementation Planning Agent"]} + status: approved +- id: FESA-REQ-NSNR-030 + statement: "The FESA solver shall pass an approved verification portfolio covering the materially linear small-displacement limit, tangent consistency, equilibrium/reaction, symmetry or objectivity, and commit/rollback behavior." + category: verification + rationale: "Convergence alone does not establish nonlinear solver correctness." + source: docs + priority: must + verification_method: analysis + acceptance_criteria: "Numerical Review defines blocking cases and quantities for every listed category, and implementation passes each approved analytical, invariant, physics, or comparison gate." + tolerance: "Case-specific tolerances are owned by Numerical Review; existing linear-limit tolerance remains unchanged." + trace_to: {parent_need: "NEED-NSNR-004", downstream_agents: ["Research Agent", "Formulation Agent", "Numerical Review Agent"]} + status: approved +- id: FESA-REQ-NSNR-034 + statement: "The FESA solver shall compare only approved accepted-state quantities against stored reference artifacts using stable source/component matching and the common docs/TOLERANCE.md policy." + category: verification + rationale: "Reference acceptance must be deterministic and independent of solver execution." + source: docs + priority: must + verification_method: reference-comparison + acceptance_criteria: "Numerical Review selects the exact existing input and required CSV quantities; precheck rejects missing, extra, duplicate, or nonfinite required rows before blocking/warning family comparison, without averaging or row-order matching." + tolerance: "docs/TOLERANCE.md family-scale policy; exact artifacts and families are a Numerical Review-owned readiness gap." + trace_to: {parent_need: "NEED-NSNR-004", downstream_agents: ["Numerical Review Agent", "I/O Definition Agent"]} + status: approved +``` + +## 9. Verification Quantities +| quantity | dimension / coordinates | role | +| --- | --- | --- | +| nodal displacement and committed rotation/director state | length and dimensionless rotation; global | accepted-state kinematics and rollback | +| full residual and constrained reaction | force or force-length; global DOF | equilibrium and reaction evidence | +| MITC4 internal force, stress and strain | model-consistent dimensions; approved element frame/configuration | formulation, physics and reference verification | +| scalar load factor and accepted frame identity | dimensionless | path, commit and output ordering | +| four convergence channels | typed as NSNR-069/070 | internal iteration acceptance only | +| iteration summary | diagnostic identity, not a physical reference quantity | convergence/failure audit | + +## 10. Tolerance Policy +- `.inp` values remain in the user's consistent unit system; FESA performs no unit inference or conversion. +- Only nonzero-scale convergence ratios are dimensionless and pass with `<=1e-2`. +- Exact-zero residual thresholds are `1e-3` force and `1e-3` force-length; correction thresholds are `1e-3` length and `1e-3` dimensionless rotation. Equal literals do not merge their dimensions. +- External comparisons use `docs/TOLERANCE.md`; internal invariant, tangent, endpoint-arithmetic and physics tolerances are fixed by Numerical Review before implementation. + +## 11. Reference Case Requirements +- The current Stage-1 gap is selection of exact stored nonlinear input and only the CSV quantities required for acceptance. +- Numerical Review owns artifact readiness, blocking/warning families, source/component identity and HDF5 projection; this gap does not require another Stage-1 user question. +- Agents do not run Abaqus, Nastran or another reference solver and do not create, rename, repair or normalize stored reference artifacts. + +## 12. Requirement Verification Matrix +| id | category | source | priority | method | compact acceptance | tolerance | downstream | status | +| --- | --- | --- | --- | --- | --- | --- | --- | --- | +| `NSNR-001` | functional | user | must | test | exactly one supported source/semantic nonlinear step | exact cardinality | I/O; Planning | approved | +| `NSNR-003` | physics | user | must | test | MITC4 geometric-only, linear isotropic material | exact inventory | Research; Formulation; Numerical Review | approved | +| `NSNR-041` | physics | user | must | analysis | fixed initial reference, no re-basing | identity exact | Research; Formulation; Numerical Review | approved | +| `NSNR-074` | physics | user | must | analysis | finite committed/trial triad/director state and rollback | invariant tolerance downstream | Formulation; Numerical Review | approved | +| `NSNR-006` | numerical | user | must | test | same-trial residual/tangent and fresh factorization/solve | identity/order exact | Formulation; Numerical Review; Planning | approved | +| `NSNR-007` | numerical | user | must | test | all four free-DOF gates pass; constrained residual is reaction | NSNR-069/070 | Numerical Review; Planning | approved | +| `NSNR-069` | numerical | user | must | test | force/moment residual relative or typed zero-scale gates | `1e-2`; typed `1e-3` | Numerical Review; Planning | approved | +| `NSNR-070` | numerical | user | must | test | translation/rotation correction relative or typed zero-scale gates | `1e-2`; typed `1e-3` | Numerical Review; Planning | approved | +| `NSNR-008` | numerical | user | must | test | finite data, iterations 1..100, pass at 100 allowed | predicates/count exact | Numerical Review; Planning | approved | +| `NSNR-014` | constraint | user | must | test | unchanged full correction; no line search/fallback/energy gate | identity exact | Numerical Review; Planning | approved | +| `NSNR-046` | numerical | user | must | test | fixed increment, final shortening, no retry | factor/order exact | Numerical Review; Planning | approved | +| `NSNR-048` | physics | user | must | test | one proportional factor for all load/BC targets | identity exact | Formulation; Numerical Review | approved | +| `NSNR-018` | physics | user | must | test | fixed-global dead force/moment and no follower tangent | component exact | Formulation; Numerical Review | approved | +| `NSNR-063` | physics | user | must | test | absolute factor-one BC target and separate correction | path/source exact | Formulation; Numerical Review | approved | +| `NSNR-016` | input | user | must | test | four-value STATIC mapping and validation | endpoint exact | I/O; Planning | approved | +| `NSNR-011` | functional | user | must | test | separate trial, atomic commit, prior-state preservation | state exact | Formulation; Numerical Review; Planning | approved | +| `NSNR-019` | physics | docs | must | test | stable source/assembly and full-equilibrium residual/reaction | identity/order exact | Formulation; Numerical Review; I/O | approved | +| `NSNR-020` | input | docs | must | test | unsupported meaning fails closed | inventory exact | I/O; Planning | approved | +| `NSNR-021` | output | user | must | test | accepted commit/frame bijection and failure-safe HDF5 final | identity exact | Numerical Review; I/O; Planning | approved | +| `NSNR-024` | output | user | must | test | one ordered diagnostic summary per entered iteration and persistent live log | semantic identity exact | I/O; Planning | approved | +| `NSNR-083` | output | user | must | test | repository names; every literal --output form unrecognized with pre-input/pre-Analysis/pre-output exit 2 and no alias/deprecation; asymmetric lifecycle; linear regression | public identity/precedence exact | I/O; Planning; Numerical Review | approved | +| `NSNR-026` | constraint | docs | must | test | deterministic factor/iteration/assembly/frame/result/log order | discrete order exact | Numerical Review; Planning | approved | +| `NSNR-030` | verification | docs | must | analysis | blocking small-limit/tangent/physics/rollback portfolio | case-specific downstream | Research; Formulation; Numerical Review | approved | +| `NSNR-034` | verification | docs | must | reference-comparison | stored artifacts, deterministic matching and precheck | docs/TOLERANCE.md | Numerical Review; I/O | approved | + +## 13. Open Questions +없음. Specialist gaps are owned by downstream stages and are escalated only if they would change approved scope, physics, tolerance, authoritative output or public compatibility. + +## 14. Downstream Handoff +- Research/Formulation: exact Total Lagrangian MITC4 equations, strain/stress measures, rotation map/side/frame, drilling and consistent derivatives. +- Numerical Review: endpoint arithmetic, tangent/objectivity/state-invariant checks, benchmark portfolio, performance adequacy and exact reference artifacts/quantities. +- I/O Definition: HDF5 schema/projection/chunking/factor-0 handling, log representation/failure presentation and path/collision conventions. +- Implementation Planning: backend adapters, output ownership primitive, candidate filename, performance targets and requirement-traced TDD plan. +- Coordinator: escalate only a downstream proposal that changes the approved scope, physics, convergence tolerance, authoritative-result meaning or public output contract; do not advance the workflow on this document alone. diff --git a/docs/nonlinear-static-newton-raphson/research.md b/docs/nonlinear-static-newton-raphson/research.md new file mode 100644 index 0000000..e20f517 --- /dev/null +++ b/docs/nonlinear-static-newton-raphson/research.md @@ -0,0 +1,602 @@ +# Nonlinear Static Newton–Raphson 연구 브리프 + +## 1. Metadata + +- feature_id: `nonlinear-static-newton-raphson` +- source_requirement: `docs/nonlinear-static-newton-raphson/requirements.md` +- source_requirement_status: `approved` +- source_requirement_approval_date: `2026-08-23` +- status: `passed` +- owner_agent: `research-agent` +- date: `2026-08-23` +- research_scope: materially linear, geometrically nonlinear Total Lagrangian + `S4/S4R -> FESA-MITC4`, finite rotation, Full Newton, fixed proportional path, + state/output integrity, and verification evidence +- evidence_boundary: 이 문서는 정식화, 수치 허용오차, C++ API, I/O schema 또는 + reference artifact를 확정하지 않는다. 외부 solver의 공개 결과는 후보 수치 evidence일 + 뿐 내부 알고리즘 동등성 evidence가 아니다. + +이 문서의 주장은 다음 네 가지 표지를 사용한다. + +- **Verified fact**: 인용한 원문·공식 문서가 직접 뒷받침한다. +- **Project decision**: 승인된 요구조건 또는 프로젝트 전역 계약이 고정한다. +- **Inference**: verified fact와 project decision에서 도출한 연구 해석이며 downstream + 재검토가 필요하다. +- **Open issue**: evidence 또는 downstream 결정이 아직 없다. + +## 2. Research Questions + +승인된 `FESA-REQ-NSNR-003`, `FESA-REQ-NSNR-041`, `FESA-REQ-NSNR-074`, +`FESA-REQ-NSNR-006`, `FESA-REQ-NSNR-048`, `FESA-REQ-NSNR-018`, +`FESA-REQ-NSNR-063`, `FESA-REQ-NSNR-011`, `FESA-REQ-NSNR-019`, +`FESA-REQ-NSNR-030`, `FESA-REQ-NSNR-034`의 specialist gap에서 다음 질문을 도출했다. + +1. 고정 초기 참조면을 쓰는 Total Lagrangian 4-node Reissner–Mindlin/MITC4 shell에서 + materially linear response를 표현할 때 어떤 strain/stress/virtual-work 근거가 필요한가? +2. committed/trial triad와 director를 multiplicative finite-rotation update로 갱신할 때 + orthonormality뿐 아니라 objectivity, path independence, singularity avoidance와 consistent + linearization을 어떻게 별도로 입증해야 하는가? +3. 기존 linear MITC4의 `24 global -> 20 physical + 4 numerical drill` 경계를 finite rotation에 + 확장할 때 global map의 1·2차 미분, rotation chart/recentering, objective drilling potential과 + nodal-moment work 중 무엇이 아직 미해결인가? +4. Full Newton에서 residual, algorithmic tangent, factorization과 correction이 같은 trial + state를 가리킨다는 것을 어떤 수학적·실행 순서 evidence로 확인할 수 있는가? +5. fixed-global dead `CLOAD`와 absolute prescribed `BOUNDARY`를 하나의 scalar factor로 + 진행할 때 translation, finite rotation, reaction과 external work의 의미는 무엇인가? +6. original MITC4의 shear/membrane locking, distorted geometry, drilling, quadrature와 + conditioning 위험을 nonlinear large-rotation 상태에서 어떻게 제한하고 특성화할 것인가? +7. small-displacement limit, tangent consistency, equilibrium/reaction, rigid-body/objectivity, + symmetry, deterministic commit/rollback을 서로 독립적으로 검증할 benchmark/patch/MES/MMS + portfolio는 무엇인가? +8. 공개 benchmark와 기존 저장 artifact 중 정확히 어떤 입력·target quantity가 현재 + 사용 가능하며, 무엇이 nonlinear acceptance artifact로는 아직 비어 있는가? + +| research question | requirement_ids | research gap | +| --- | --- | --- | +| RQ-1 | `FESA-REQ-NSNR-003`, `FESA-REQ-NSNR-041` | TL materially-linear MITC4 theory boundary | +| RQ-2 | `FESA-REQ-NSNR-074` | multiplicative triad/director update, objectivity and derivatives | +| RQ-3 | `FESA-REQ-NSNR-003`, `FESA-REQ-NSNR-074` | nonlinear global/physical/drill map and finite nodal-moment work | +| RQ-4 | `FESA-REQ-NSNR-006` | same-trial Full Newton consistency evidence | +| RQ-5 | `FESA-REQ-NSNR-048`, `FESA-REQ-NSNR-018`, `FESA-REQ-NSNR-063` | proportional dead-load/prescribed finite path | +| RQ-6 | `FESA-REQ-NSNR-003` | locking, drilling, quadrature and conditioning limits | +| RQ-7 | `FESA-REQ-NSNR-011`, `FESA-REQ-NSNR-019`, `FESA-REQ-NSNR-030` | physics, tangent, objectivity and transactional verification portfolio | +| RQ-8 | `FESA-REQ-NSNR-034` | exact stored/public nonlinear artifact and target readiness | + +## 3. Source Inventory + +### 3.1 Project contracts and local evidence + +Project contract는 외부 reliability tier와 혼합하지 않고 `Project`로 표시한다. + +| id | source_type | title/path | reliability_tier | 사용 범위와 한계 | +| --- | --- | --- | --- | --- | +| P1 | approved requirement | `docs/nonlinear-static-newton-raphson/requirements.md` | Project | 승인 scope, load path, Newton/state/output/verification 계약. 정식 방정식·내부 tolerance·exact reference artifact는 고정하지 않음 | +| P2 | project governance | `AGENTS.md`, `docs/SOLVER_AGENT_DESIGN.md`, `docs/PRD.md` | Project | 독립 solver 정체성, 8-stage gate, research ownership과 external-reference 경계 | +| P3 | architecture/decision | `docs/ARCHITECTURE.md`, `docs/ADR.md` (`ADR-016`, `ADR-017`, `ADR-022`) | Project | 별도 nonlinear procedure, deterministic assembly, candidate-before-commit, full residual/reaction 및 공통 comparison 정책. nonlinear shell 방정식은 없음 | +| P4 | tolerance policy | `docs/TOLERANCE.md` | Project | 저장 reference row precheck와 family-scale row/RMS gate. tangent/objectivity/orthonormality/iteration tolerance를 제공하지 않음 | +| P5 | existing linear MITC4 evidence | `docs/linear-static-mitc4-shell/{research,formulation,numerical-review,reference-model}.md` | Project | 승인된 linear MITC4 물리/적분/결과 경계와 기존 test inventory. `formulation.md` §15는 future-only gap inventory이며 nonlinear 정식화 evidence가 아님 | +| P6 | local tests/artifacts | `tests/unit/elements/mitc4_shell_test.cpp`, `tests/unit/model/shell_geometry_test.cpp`, `tests/reference/mitc4_reference_cases_test.cpp`, `tests/reference/mitc4_reference_comparison_test.cpp`, `reference/shell/`, `reference/shellR/` | Project | linear rigid/patch/geometry/reference 회귀의 exact local identity. 두 `.inp` 모두 `nlgeom=NO`; nonlinear acceptance-ready가 아님 | + +### 3.2 External sources + +- access_date: `2026-08-23` (`S1`–`S17` 공통) +- tier_policy: Tier 1은 공식 표준·기관·solver manual, Tier 2는 peer-reviewed 원 논문·교과서, + Tier 3는 탐색용 synthesis를 뜻한다. + +| id | source_type | title | author_or_org | URL_or_DOI | reliability_tier | 제공 evidence / 접근·적용 한계 | +| --- | --- | --- | --- | --- | --- | --- | +| S1 | peer-reviewed original paper | *A Continuum Mechanics Based Four-Node Shell Element for General Non-linear Analysis* | E. N. Dvorkin, K.-J. Bathe | [MIT author PDF](https://web.mit.edu/kjb/www/Publications_Prior_to_1998/A_Continuum_Mechanics_Based_Four-Node_Shell_Element_for_General_Nonlinear_Analysis.pdf), DOI [`10.1108/eb023562`](https://doi.org/10.1108/eb023562) | Tier 2 | original four-node continuum-based shell, Total Lagrangian nonlinear equations, assumed transverse shear, examples, `2x2x2` elastic integration. 1984 five-physical-DOF update이며 FESA global 24-DOF/drill 계약은 없음; PDF는 공개 author copy이나 저작권 자료 | +| S2 | peer-reviewed original paper | *On a Stress Resultant Geometrically Exact Shell Model. Part III: Computational Aspects of the Nonlinear Theory* | J. C. Simo, D. D. Fox, M. S. Rifai | [publisher record](https://www.sciencedirect.com/science/article/pii/0045782590900943), DOI [`10.1016/0045-7825(90)90094-3`](https://doi.org/10.1016/0045-7825(90)90094-3) | Tier 2 | singularity-free exact director update, finite-deformation mixed fields, exact discrete-equilibrium linearization, nonlinear examples. stress-resultant shell model이므로 FESA 식의 직접 근거가 아니며 publisher full text 접근 제한 가능 | +| S3 | peer-reviewed original paper | *On the Choice of Finite Rotation Parameters* | A. Ibrahimbegović | [publisher record](https://www.sciencedirect.com/science/article/pii/S0045782597000595), DOI [`10.1016/S0045-7825(97)00059-5`](https://doi.org/10.1016/S0045-7825(97)00059-5) | Tier 2 | finite-rotation parametrization과 incremental rotation/Newton 구현 선택의 영향. 일반 구조 rotation 논문이며 MITC4/drilling 특화가 아님 | +| S4 | peer-reviewed original paper | *Multiplicative Updating of the Rotation Tensor in the Finite Element Analysis of Rods and Shells—A Path Independent Approach* | C. Sansour, W. Wagner | [institutional record](https://digital.library.adelaide.edu.au/items/e3451786-5c76-498e-a1cd-662e73db573f), DOI [`10.1007/s00466-002-0401-4`](https://doi.org/10.1007/s00466-002-0401-4) | Tier 2 | multiplicative update의 path-dependence 문제와 path-independent 접근. Cosserat-type rod/shell이며 FESA의 numerical drill potential을 정의하지 않음 | +| S5 | peer-reviewed open-access review/original formulation | *A Consistent Finite Element Formulation of the Geometrically Non-linear Reissner–Mindlin Shell Model* | A. Müller, M. Bischoff | [Springer open access](https://doi.org/10.1007/s11831-021-09702-7); corrections [`10.1007/s11831-022-09725-8`](https://doi.org/10.1007/s11831-022-09725-8), [`10.1007/s11831-022-09832-6`](https://doi.org/10.1007/s11831-022-09832-6) | Tier 2 | director가 사는 nonlinear manifold, objective/path-independent interpolation, potential의 correct gradient/Hessian 필요성. CC BY 4.0; projection-based higher-order formulation은 FESA MITC4와 다름 | +| S6 | peer-reviewed original paper | *The MITC4+ Shell Element in Geometric Nonlinear Analysis* | Y. Ko, P.-S. Lee, K.-J. Bathe | [MIT author PDF](https://web.mit.edu/kjb/www/Principal_Publications/The_MITC4%2B_shell_element_in_geometric_nonlinear_analysis.pdf), DOI [`10.1016/j.compstruc.2017.01.015`](https://doi.org/10.1016/j.compstruc.2017.01.015) | Tier 2 | TL/Green–Lagrange nonlinear MITC4+, quaternion triad update, `2x2x2` integration, analytical/FE benchmarks, distorted-mesh locking evidence. MITC4+는 assumed membrane field를 추가한 다른 element이며 graph-only target이 많음 | +| S7 | official solver theory manual | [Nonlinear Solution Methods in Abaqus/Standard](https://docs.software.vt.edu/abaqusv2024/English/SIMACAETHERefMap/simathe-c-nonlinearsol.htm) | Dassault Systèmes | official 2024 documentation | Tier 1 | Newton Jacobian/residual/correction의 same-state 관계, full/modified/quasi-Newton 구분, residual+correction checks. Abaqus adaptive controls와 approximations는 P1이 배제하며 내부 동등성 근거가 아님 | +| S8 | official solver benchmark | [3DNLG-1: Elastic Large Deflection Response of a Z-Shaped Cantilever Under an End Load](https://docs.software.vt.edu/abaqusv2025/English/SIMACAEBMKRefMap/simabmk-c-3dnlg1.htm) | Dassault Systèmes / NAFEMS attribution | official 2025 documentation; NAFEMS R0024 | Tier 1 | 공개 S4/S4R input 이름, 재료/BC/load, 세 load level의 tip displacement와 moment-at-A 표. 페이지가 NAFEMS 권고 문제를 재현하지만 source independence와 FESA subset 적합성은 별도 확인 필요 | +| S9 | official solver benchmark | [3DNLG-9: Large Elastic Deflection of a Pinched Hemispherical Shell](https://docs.software.vt.edu/abaqusv2024/English/SIMACAEBMKRefMap/simabmk-c-3dnlg9.htm) | Dassault Systèmes / NAFEMS attribution | official 2024 documentation; NAFEMS R0024 | Tier 1 | 공개 S4/S4R input 이름, point-load/symmetry 조건, 세 load level의 A/B radial displacement 표. 공식 페이지가 NAFEMS 공개값이 Abaqus로 얻어졌음을 명시하므로 Abaqus와 NAFEMS 표의 비교는 독립 검증이 아님 | +| S10 | official benchmark catalog | [Geometric Non-linearity benchmark catalog](https://www.nafems.org/publications/glossaryofbenchmarks/nonlinear/geometric/), [R0029 record](https://www.nafems.org/publications/resource_center/r0029/) | NAFEMS | publication `R0029` / summary `R0024` | Tier 1 | 3D beam/shell geometric-nonlinear benchmark inventory와 목적. exact R0029 report는 유료여서 이번 연구에서 전체 원문·독립 source tables를 확인하지 못함 | +| S11 | official standard | *V&V 10-2019 (R2025), Standard for Verification and Validation in Computational Solid Mechanics* | ASME | [official record](https://www.asme.org/codes-standards/find-codes-standards/standard-for-verification-and-validation-in-computational-solid-mechanics) | Tier 1 | V&V/VVUQ 공통 framework와 용어. 유료 full standard 미열람이므로 분류 수준으로만 사용하고 세부 acceptance를 귀속하지 않음 | +| S12 | government report | *Code Verification by the Method of Manufactured Solutions* | K. Salari, P. K. Knupp, Sandia National Laboratories | [Sandia record](https://www.sandia.gov/research/publications/details/code-verification-by-the-method-of-manufactured-solutions-2000-06-01/), DOI [`10.2172/759450`](https://doi.org/10.2172/759450), `SAND2000-1444` | Tier 1 | MMS가 order-of-accuracy에 영향을 주는 coding error를 탐지할 수 있다는 방법론과 blind tests. 예제는 주로 CFD이며 shell input/target을 제공하지 않음 | +| S13 | peer-reviewed paper + reproducible artifact | *Method of Manufactured Solutions Code Verification of Elastostatic Solid Mechanics Problems in a Commercial Finite Element Solver* | K. I. Aycock, N. Rebelo, B. A. Craven | [publisher record](https://www.sciencedirect.com/science/article/pii/S0045794919301968), DOI [`10.1016/j.compstruc.2019.106175`](https://doi.org/10.1016/j.compstruc.2019.106175), artifact DOI [`10.6084/m9.figshare.7726352.v2`](https://doi.org/10.6084/m9.figshare.7726352.v2) | Tier 2 | elastostatic small/finite-strain MMS source-generation notebook와 input artifact. 3-D solid/body-source 및 다른 constitutive cases라 현재 MITC4/CLOAD/BOUNDARY subset에 직접 실행 불가 | +| S14 | official solver verification guidance | [About Element Verification](https://docs.software.vt.edu/abaqusv2024/English/SIMACAEVERRefMap/simaver-c-basicelemover.htm) | Dassault Systèmes | official 2024 documentation | Tier 1 | patch test만으로 shell을 충분히 검증할 수 없고 geometric-nonlinear element에 constant-strain/rigid-rotation checks가 필요하다는 vendor verification 관행. FESA acceptance 수치나 내부 등가성은 제공하지 않음 | +| S15 | configured FEM wiki navigation | `Nonlinear Finite Element Analysis`, `MITC4 Shell Element`, `MITC Shell Kinematics`, `Green-Lagrange Strain Linearization`, `Shell Locking Phenomenon`, `Shell Element Benchmark Testing`, `Scordelis-Lo Shell Benchmark` | MultiPhysicsVault | local `C:\git\MultiPhysicsVault\wiki\` | Tier 3 | source 탐색과 용어 연결에만 사용. 핵심 주장은 P1–P6 또는 S1–S14/S16–S17 원문으로 추적함 | +| S16 | peer-reviewed benchmark paper + institutional postprint | *Popular Benchmark Problems for Geometric Nonlinear Analysis of Shells* | K. Y. Sze, X. H. Liu, S. H. Lo | [HKU institutional record and postprint](https://hub.hku.hk/handle/10722/54269), DOI [`10.1016/j.finel.2003.11.001`](https://doi.org/10.1016/j.finel.2003.11.001) | Tier 2 | eight benchmark sets의 geometry/load와 dense tabulated load–deflection data, mesh refinement 및 equal-increment difficulty evidence. CC BY-NC-ND institutional postprint; 값은 Abaqus S4R 계산이고 vendor Updated-Lagrangian/reduced-integration/hourglass/drill 및 automatic-control 결과이므로 FESA formulation이나 독립 reference와 동일시할 수 없음 | +| S17 | official solver verification example | [Rigid Body Motion Output Variables](https://docs.software.vt.edu/abaqusv2024/English/SIMACAEVERRefMap/simaver-c-rigidbodymotoutput.htm) | Dassault Systèmes | official 2024 documentation | Tier 1 | `xrbmshel.inp`가 shell elements에 imposed 90-degree z-axis rigid rotation을 가하고 rigid-body output을 확인함. direct-integration implicit dynamics와 vendor whole-set output test라 FESA nonlinear-static strain/internal-force objectivity artifact가 아님 | + +## 4. Extracted Facts and Theory Summary + +### 4.1 Total Lagrangian four-node shell boundary + +- **Verified fact — S1/S6:** Dvorkin–Bathe 계열의 continuum-based four-node shell은 + midsurface translation과 nodal director rotation으로 shell continuum를 나타내며, + Total Lagrangian 기술에서 초기 configuration에 대한 Green–Lagrange strain 계열과 그에 + work-conjugate한 stress를 사용해 internal virtual work를 구성한다. S6는 이 계열을 + geometric nonlinear MITC4+로 전개하고 incremental Green–Lagrange strain을 residual/tangent + 계산에 사용한다. +- **Project decision — P1:** FESA는 하나의 고정 초기 reference를 유지하고 homogeneous + isotropic materially linear law만 허용한다. 따라서 material state/history 없이 geometry와 + rotation에서만 비선형성이 생겨야 한다. +- **Inference:** Formulation은 동일 trial state에서 initial-reference geometry, current + midsurface, current director/triad, strain, materially linear stress와 internal virtual work가 + 연결되는 한 계통을 제시해야 한다. 정확한 strain components, plane-stress reduction, + thickness assumption, stress/resultant recovery는 이 연구가 확정하지 않는다. +- **Verified fact — S1/S6:** original MITC4의 assumed covariant transverse-shear interpolation은 + thin-shell shear locking을 줄이기 위한 핵심이다. S6의 nonlinear 계산은 네 node shell에 + `2 x 2 x 2` Gauss integration을 사용한다. +- **Project decision — P5:** 기존 승인 linear FESA-MITC4도 source `S4/S4R` 모두 하나의 + `2 x 2` midsurface × two-point-thickness 경로와 동일 MITC shear tying을 쓴다. source label은 + Abaqus S4/S4R integration 선택자가 아니다. +- **Inference:** 기존 rule을 nonlinear trial geometry에 그대로 “호출”하는 것만으로 consistent + TL element가 되지 않는다. 각 quadrature/tying 위치의 reference/current frame, strain variation, + stress-resultant와 geometry/map Hessian을 재유도해야 한다. `P5` §15는 이 필요사항의 목록이지 + 승인된 해답이 아니다. +- **Applicability fact — S1/S6:** 이 shell family의 large displacement/rotation 사용은 thin-to-thick + Reissner–Mindlin-type kinematics와 small elastic strain 가정 안에서 해석해야 한다. materially + linear law를 큰 material strain의 물리 모델로 일반화할 evidence는 없다. + +### 4.2 Finite rotations, director and objectivity + +- **Verified fact — S2/S3/S5:** finite rotation은 additive Euclidean vector가 아니며, + configuration update, interpolation과 linearization은 rotation/director가 놓인 nonlinear + manifold를 반영해야 한다. S2는 magnitude와 무관한 singularity-free director update와 exact + discrete linearization을, S5는 objective/path-independent director interpolation과 correct + potential gradient/Hessian의 필요성을 제시한다. +- **Verified fact — S4:** rotation tensor를 단순히 multiplicative하게 누적한다는 사실만으로 + path independence가 자동 보장되지 않는다. update의 interpolation/parameterization과 state + 정의를 함께 검토해야 한다. +- **Project decision — P1:** 각 node에는 committed/trial orthonormal right-handed triad `Q`가 + 있고 director는 세 번째 축이다. correction은 dimensionless이며 update는 multiplicative다. +- **Inference:** 적절한 proper-orthogonal incremental rotation을 곱하면 한 번의 연산은 triad의 + orthonormality와 handedness를 보존할 수 있다. 그러나 left/right multiplication, spatial/body + increment convention, exponential/quaternion map, small-angle branch, accumulated chart의 + recentering과 derivative를 고정하지 않으면 residual/tangent/BC/moment가 유일해지지 않는다. +- **Open issue O-ROT-01:** Formulation이 `Q_trial` update의 multiplication side, increment frame, + retraction과 first/second directional derivative를 정해야 한다. 이것은 approved “multiplicative” + 의미를 구체화하되 global DOF/public input 의미를 바꾸어서는 안 된다. +- **Open issue O-ROT-02:** nodal director/triad에서 Gauss/tying point director와 frame을 만드는 + objective interpolation, normalization derivative 및 degenerate/opposed director의 fail-closed + 조건이 아직 없다. S5의 특정 projection-based interpolation을 FESA가 채택한다고 추론하지 않는다. +- **Inference:** objectivity는 단지 최종 `Q^T Q=I`, `det(Q)=+1` 검사와 다르다. initial/current + geometry와 모든 triad에 같은 finite rigid motion을 superpose했을 때 physical strain/stress, + internal energy와 equilibrium law가 적절히 invariant/covariant해야 한다. + +### 4.3 Global 24 DOFs, drilling and nodal moments + +- **Verified fact — S1:** original continuum-based four-node shell은 node당 두 director rotation을 + 쓰는 five-physical-DOF element로 제시된다. director 축 주위 rotation은 original physical + shell strain이 아니다. +- **Project decision — P1/P5:** FESA public/global field는 node당 세 `UR`을 유지하고, 기존 + linear element는 director-tangent physical pair와 director-parallel numerical drill coordinate를 + 분리한다. fixed small diagonal drill stabilization은 linear 계약에서만 승인되었다. +- **Inference:** finite rotation에서 current director에 대한 “parallel/tangent” projection 자체가 + state-dependent하다. 그러므로 physical 20-coordinate residual을 global 24-coordinate correction에 + 옮기는 map의 첫 미분뿐 아니라 map의 변화가 만드는 second-derivative/geometric term까지 + consistent tangent에 필요하다. +- **Open issue O-DRILL-01:** objective nonlinear drilling potential, rotating reference, stiffness + scale의 committed/trial 의존성, residual과 exact Hessian이 없다. linear diagonal을 current + coordinates에 그대로 더하면 large rigid rotation에 artificial energy를 만들 수 있다는 것은 + **inference**이며, Formulation/Numerical Review가 potential 수준에서 판정해야 한다. +- **Verified boundary — S4/S5:** path-independent/objective shell formulations 또는 physical + Cosserat drilling rotation은 존재하지만, 그것은 FESA의 numerical drill regularization과 다른 + 물리 모델이다. 이를 근거로 FESA drill을 physical strain/load channel로 바꿀 수 없다. +- **Open issue O-MOM-01:** fixed-global dead nodal moment의 components는 P1이 고정하지만, + multiplicative rotation correction과 work-conjugate generalized moment, virtual work, consistent + derivative는 아직 없다. “follower-load tangent 없음”이 “rotation-map derivative도 없음”을 + 뜻한다고 추론해서는 안 된다. +- **Open issue O-DRILL-02:** current director와 평행한 applied moment의 거부/허용 projection이 + finite state에서 어떻게 평가되는지, physical moment work와 numerical drill을 어떻게 완전히 + 분리하는지 downstream 계약이 필요하다. + +### 4.4 Full Newton and same-trial consistent tangent + +- **Verified fact — S7:** Newton linearization은 현재 iterate에서 평가한 equilibrium residual과 + 그 residual의 Jacobian을 같은 state에서 사용한다. full Newton은 매 iteration Jacobian을 다시 + 형성하고 푸는 방법이며, residual과 correction을 함께 작게 확인하는 것이 일반적이다. +- **Project decision — P1:** FESA는 residual과 algorithmically consistent tangent를 같은 trial + identity에서 평가하고, entered iteration마다 fresh factorization/solve를 하며, correction을 + 변경 없이 적용한다. iteration `1..100`, fixed increments, no line search/damping/cutback/retry다. +- **Inference:** “material tangent + geometric stiffness”라는 이름의 합만으로 consistency가 + 입증되지 않는다. 선택한 rotation retraction 아래에서 physical internal force, state-dependent + 24/20 map, drilling potential, prescribed-DOF elimination과 external work를 모두 방향미분한 결과가 + assembled residual의 Jacobian과 일치해야 한다. +- **Inference:** fixed-global translational dead force의 magnitude/direction은 displacement와 무관하므로 + translation virtual-work 표현이 additive global translation이면 그 load contribution은 configuration + derivative를 만들지 않는다. 이 결론은 nodal moment나 prescribed finite rotation에 자동 확장되지 + 않는다. +- **Inference / verification consequence — S7/P1:** deterministic directional-derivative test에서 동일 trial state와 동일 + rotation retraction을 사용해 `K p`를 centered residual difference와 비교해야 한다. perturbation을 + 한 값으로 고정해 우연한 cancellation을 통과시키지 말고 truncation/roundoff plateau를 확인하되, + perturbation grid와 tolerance는 Numerical Review가 정한다. +- **Inference / symmetry boundary — S5/P1:** materially linear conservative internal potential과 conservative numerical + drilling potential을 정확히 두 번 미분한 적절한 coordinate Hessian은 symmetry 후보가 된다. + 그러나 nodal moment work, rotation coordinate choice와 constraint reduction이 미정이므로 complete + global tangent symmetry를 이 연구에서 요구사항 이상으로 확정하지 않는다. + +### 4.5 Proportional loads and prescribed paths + +- **Project decision — P1:** 모든 approved `CLOAD`와 nonzero `BOUNDARY`는 step-start에서 factor-one + target까지 같은 scalar factor를 쓰고, factor는 fixed positive increment와 마지막 shortening만으로 + 정확히 1에 도달한다. `CLOAD` force/moment는 global direction이 고정된 dead load다. +- **Project decision — P1:** prescribed value는 factor-one absolute global-DOF target이며 Newton + correction과 다르다. constrained component는 convergence norm에서 빠지지만 complete assembled + residual의 constrained entry는 reaction 의미를 가진다. +- **Open issue O-BC-01:** finite rotational `BOUNDARY` target을 `Q_start`에 상대적인 rotation vector로 + 해석하는지, `Q(lambda)`를 어떤 retraction/side로 구성하는지, constrained correction과 target + mismatch를 어떤 coordinate에서 계산하는지 Formulation이 정해야 한다. +- **Inference:** Cartesian nodal positions를 `X + lambda (R-I)X`로 선형 보간하는 prescribed path는 + 일반적으로 중간 `lambda`에서 exact rigid rotation 궤적이 아니다. 따라서 finite rigid-body + objectivity test를 단순 proportional displacement BC로 만들면 중간 상태에 strain이 생길 수 있다. + operator-level superposition test 또는 처음부터 rigidly transformed 된 두 독립 모델의 covariance + 비교가 더 직접적인 후보이며, exact rigid prescribed path를 새 public 의미로 추가하면 scope change다. +- **Inference / applicability consequence — P1:** limit point, snap-through/post-buckling branch, follower pressure와 + non-proportional control이 필요한 benchmark는 첫 release의 acceptance 후보가 아니다. fixed-load + increment가 Newton attraction radius 밖이면 deterministic failure가 맞으며, automatic cutback을 + 기대할 수 없다. + +### 4.6 Locking, integration and geometry risks + +- **Verified fact — S6:** original MITC4는 transverse shear를 MITC 방식으로 처리하지만 membrane + strain을 MITC4+처럼 보강하지 않는다. curved 또는 response 중 distorted mesh에서는 membrane + locking으로 load–displacement accuracy가 크게 저하될 수 있다. +- **Project decision — P5:** FESA `S4`와 `S4R`는 같은 original-style MITC4 path다. Abaqus S4/S4R의 + full/reduced integration, hourglass, membrane enhancement 또는 stabilization 차이를 상속하지 않는다. +- **Inference:** `2x2x2` common rule은 S1/S6 및 linear FESA와 연결되는 강한 candidate지만, + nonlinear strain/tangent의 각 항을 어느 위치에서 적분할지는 Formulation이 source 식으로 + 확인해야 한다. one-point reduction/hourglass control을 source `S4R` 때문에 도입할 근거는 없다. +- **Verified risk / inference — S6/P5:** thin/slender geometry, curved/distorted quads, nearly degenerate positive Jacobian과 작은 + drill scale은 locking 또는 conditioning을 악화할 수 있다. current trial geometry가 심하게 + 변형되어도 TL reference mapping과 current frame/director 모두 각 required Gauss/tying/recovery + 위치에서 finite/valid해야 한다. +- **Inference / verification consequence — S6/P1:** regular/distorted, thickness/radius 또는 thickness/length sequence를 + 함께 보고, 단일 point response가 맞는 것만으로 locking-free를 주장하지 않는다. MITC4+ + convergence를 original FESA-MITC4 acceptance target으로 사용하지 않는다. + +### 4.7 Equilibrium, reactions and transactional state + +- **Project decision — P1/P3:** full assembled equilibrium at a trial/accepted state gives free-DOF + residual and constrained reaction. stable source/component identity와 deterministic assembly/reduction + order를 보존해야 한다. +- **Inference:** accepted state 검증은 free residual norm만이 아니라 fixed-global resultant force와 + moment balance를 함께 확인해야 한다. global moment balance는 한 fixed origin에 대한 nodal-force + moment, nodal couple와 reactions를 모두 포함해야 하며 exact sign/identity는 Formulation/Numerical + Review가 정한다. +- **Project decision — P1/P3:** trial state와 output candidate는 완전히 검증된 뒤 atomic commit된다. + failure는 prior committed state와 prior authoritative HDF5를 보존하고 current-run live log는 남긴다. +- **Inference / verification consequence — P1/P3:** nonconvergence, nonfinite state/recovery, factorization/solve failure와 + output-finalization failure를 서로 다른 injected failure point로 시험해야 한다. 성공 increment만 + frame과 일대일이어야 하며 trial rotation/director가 committed state를 alias하면 안 된다. + +## 5. Candidate Benchmarks and Artifact Readiness + +후보 우선순위는 `A`(required portfolio의 직접 후보), `B`(외부 solution/reference candidate), +`C`(known-limit characterization 또는 future method)이다. 아래 수치나 source table은 아직 FESA +acceptance target/tolerance로 승인된 것이 아니다. + +### B-01 — Small-displacement linear limit (`A`) + +- **Exact candidate artifact:** 현재 read-only `reference/shell/shell.inp`, + `reference/shell/shell displacements.csv`, `shell reactions.csv`, `shell stresses.csv`; 별도로 + `reference/shellR/shellR.inp`와 대응 CSV가 존재한다. 두 input 모두 `*Step, nlgeom=NO`다. +- **Artifact gap:** 동일 source identity와 supported four-value nonlinear `STATIC`을 사용하는 + approved `nlgeom=YES` input 및 nonlinear accepted-frame CSV는 없다. 기존 pair를 rename/rewrite하거나 + nonlinear reference라고 재분류해서는 안 된다. +- **Target quantities:** 충분히 작은 response에서 accepted factor-one global `U`, physical rotation/director, + reaction, physical strain/stress/resultant의 linear procedure/baseline 접근; geometric part가 사라지는 + tangent limit; source-row identity. +- **Cannot verify:** finite rotation, nonlinear load–displacement path, nonlinear convergence, objective + drilling, rollback 또는 Abaqus nonlinear agreement. +- **Assumptions/limits:** existing center deflection scale이 geometry에 비해 작은지는 model length와 + dimensionless ratio로 다시 확인해야 한다. `shellR` artifact 존재는 FESA reduced integration 또는 + nonlinear readiness 근거가 아니다. +- **Numerical Review questions:** nonlinear variant를 test-owned input으로 승인할지; 어느 linear + HDF5/CSV quantities를 baseline으로 삼을지; geometric perturbation 크기와 case-specific limit + tolerance는 무엇인지; external comparison이 아니라 cross-procedure regression으로 분류할지. + +### B-02 — Element patch and constant-state continuation (`A`) + +- **Exact candidate artifact/gap:** 기존 exact linear unit-test concepts는 + `tests/unit/elements/mitc4_shell_test.cpp`의 membrane/bending/shear/twist/rigid tests다. finite-state + patch input/expected data artifact는 없음. +- **Target quantities:** constant membrane/bending/shear states의 nodal residual, strain/stress/resultant, + patch interface equilibrium; zero-increment state에서 linear test로의 reduction; regular/rotated/distorted + mesh에서 component/sign covariance. +- **Cannot verify:** global Newton lifecycle, full large-deflection accuracy, curved-shell membrane locking, + external reference agreement. +- **Assumptions/limits:** analytical state가 chosen nonlinear shell kinematics에 정확히 representable한지 + Formulation derivation 후 확인해야 한다. all-constrained manufactured state는 solver convergence를 + exercise하지 않는다. +- **Numerical Review questions:** 어떤 exact states가 admissible한지, drill coordinate를 어떻게 zero로 + 유지할지, element vs assembly blocking 분할과 invariant tolerance. + +### B-03 — Tangent directional derivative (`A`) + +- **Exact candidate artifact/gap:** external artifact 없음. Formulation이 정한 retraction을 쓰는 + deterministic generated trial-state test가 필요하다. +- **Target quantities:** 여러 regular/distorted elements와 assembled patch에서 translation/rotation + direction `p`에 대한 complete residual difference와 `K_T p`; material, geometric, 24/20-map, + drilling, load-work contribution을 선택적으로 isolate한 error trend. +- **Cannot verify:** 물리 solution accuracy, mesh convergence 또는 benchmark response. +- **Assumptions/limits:** centered difference의 두 perturbed states가 같은 committed base와 load factor를 + 공유해야 한다. finite-difference noise 때문에 한 epsilon의 absolute comparison은 부적절하다. +- **Numerical Review questions:** perturbation schedule, norm/scaling, expected asymptotic region과 blocking + tolerance; constrained DOF와 nodal-moment case 포함 여부; complete tangent symmetry의 expected status. + +### B-04 — Finite rigid superposition/objectivity and triad invariants (`A`) + +- **Exact candidate artifact/gap:** S17 public Abaqus verification에는 shell rigid-body-motion input + `xrbmshel.inp`가 있으나 local stored artifact가 없고 FESA subset/목적이 일치하지 않는다. + S17은 direct-integration implicit-dynamic rigid-body output test이지 nonlinear-static physical + strain/internal-force objectivity test가 아니다. + FESA operator-level superposition case도 아직 없음. +- **Target quantities:** arbitrary proper rigid rotation과 translation을 initial/current geometry 및 nodal + triads에 superpose하기 전후 physical strain/stress/energy invariance, internal force/tangent covariance, + `Q^T Q`, `det(Q)`, director-third-axis identity; rigid state의 zero physical residual. +- **Cannot verify:** deformational accuracy, nonlinear load path, reaction sign 또는 external solver agreement. +- **Assumptions/limits:** proportional Cartesian BC는 exact rigid intermediate path가 아니므로 사용하지 + 않는다. numerical drill이 physical rigid motion에 energy를 만들지 않는 map이 먼저 정의되어야 한다. +- **Numerical Review questions:** state-level 또는 solved-model covariance 중 무엇을 blocking할지; + rotation magnitudes/axes, force/tangent transform와 invariant tolerances; drill residual을 physical + residual과 어떻게 분리할지. + +### B-05 — Equilibrium/reaction and symmetry pair (`A`) + +- **Exact candidate artifact/gap:** exact local nonlinear input/expected rows 없음. one-element/patch와 + mirrored multi-element model을 새 test-owned candidate로 정의해야 한다. +- **Target quantities:** accepted free residual, constrained reaction, global resultant force/moment balance; + mirrored node/source mapping 아래 displacement, triad/director, reactions와 physical output의 parity; + deterministic row/order identity. +- **Cannot verify:** absolute large-deflection accuracy 또는 tangent consistency 단독. +- **Assumptions/limits:** mirror는 orientation/connectivity와 pseudovector moment/rotation 변환을 올바르게 + 다뤄야 한다. 단순 component equality가 아니라 signed mapped equality가 필요하다. +- **Numerical Review questions:** fixed balance origin, nodal couple 포함식, blocking quantities/tolerances, + mirror connectivity rule, symmetry와 objectivity 중 요구조건의 최소 blocking 조합. + +### B-06 — Commit/rollback and deterministic event sequence (`A`) + +- **Exact candidate artifact/gap:** external physics artifact는 필요하지 않다. repository에는 nonlinear + transactional-state failure harness가 아직 없다. +- **Target quantities:** success 시 committed state/load factor/frame의 bijection; iteration-100 pass/fail + boundary; nonconvergence, nonfinite residual/tangent/correction/recovery, factorization/solve 및 HDF5 + finalization failure 후 prior displacement/triad/director/reaction/recovery/final HDF5 보존; live log의 + entered-iteration cardinality; repeated/thread configurations의 stable event/order. +- **Cannot verify:** shell physical accuracy나 external reference agreement. +- **Assumptions/limits:** failure injection은 production semantics를 바꾸지 않는 test seam이어야 한다. +- **Numerical Review questions:** floating reproducibility 수준, state snapshot 비교량, output failure를 + commit 전 어느 validation boundary에 둘지, incomplete current increment가 log에 남길 최소 evidence. + +### B-07F — End-shear cantilever with dense tabulated path (`A/B`) + +- **Exact candidate artifact:** S16 §3.1/Table 2a/Fig. 2의 public institutional postprint. + `E=1.2e6`, `nu=0`, `L=10`, `b=1`, `h=0.1`, `P0=EI/L^2=1`, `Pmax=4P0`와 + `16 x 1` S4R model의 40 equal increments에서 horizontal/vertical tip deflections를 + `P/Pmax=0.05..1.00`에 tabulate한다. +- **Artifact gap:** machine-readable nodes/elements, exact nodal force distribution, `.inp`와 stored + FESA/reference CSV가 없다. +- **Target quantities:** Table 2a의 signed `Utip/Wtip` path, tip force factor, root reactions, + current geometry/director와 Newton iteration identity. Point dead force라 O-MOM-01을 기다리지 않는 + large-rotation global-solve 후보다. +- **Cannot verify:** curved-shell membrane locking, nodal moment work, tangent derivative, objectivity 또는 + rollback 단독. S16 값은 Abaqus S4R 결과이며 독립 analytical solution이 아니다. +- **Assumptions/limits:** paper의 S4R는 FESA와 다른 Updated-Lagrangian/reduced-integration/hourglass/drill + model이다. equality는 오직 동일 physical quantity의 external numerical comparison 후보이며 internal + compatibility를 뜻하지 않는다. 논문의 default automatic NINC/NITER가 아니라 Table 2a 생성에 쓴 + equal `NINC*=40` path만 first-release fixed-step 후보와 가까운 evidence다. +- **Numerical Review questions:** postprint geometry에서 exact mesh/connectivity/load distribution을 + 재구성해도 benchmark identity를 보존하는가; Table 2a 어느 rows/components를 blocking할지; + FESA fixed Full Newton/no-line-search에서 40 increments가 traversable한지; stored artifact provenance와 + `docs/TOLERANCE.md` family를 어떻게 정할지. + +### B-07M — Pure-moment cantilever to a circular arc/full circle, MES (`A/B`) + +- **Exact candidate artifact:** S6 §3.1/Fig. 5–7/Eq. (27)의 `16 x 1` MITC4/MITC4+ cantilever와 + analytical circular-arc solution. S16 §3.2/Table 3a/Fig. 3은 `E=1.2e6`, `nu=0`, `L=12`, + `b=1`, `h=0.1`, `Mmax=2*pi*EI/L`과 `M/Mmax=0.05..1.00`의 analytical 및 S4R tip + deflections를 tabulate한다. +- **Artifact gap:** machine-readable node/element/input, exact nodal moment distribution과 stored CSV가 + 없다. FESA-approved CLOAD nodal-moment work가 아직 미정이다. +- **Target quantities:** published analytical tip-displacement functions, final circular geometry/director, + load-factor path, root reactions, Newton iterations, objectivity under a superposed rigid transform. +- **Cannot verify:** point-force behavior, curved initial geometry, membrane-locking performance, + Abaqus agreement, numerical drilling accuracy. +- **Assumptions/limits:** thin strip가 beam analytical assumptions에 충분히 접근하는 mesh/thickness가 + 필요하고, tip moment를 node들에 배분하면 analytical end resultant와 work-equivalent해야 한다. + S16의 dense S4R columns는 analytical columns의 보조 convergence evidence이지 FESA internal-equivalence + target이 아니다. S16은 equal `NINC*=80`을 썼으며 default automatic increment counts는 FESA + fixed-step behavior의 acceptance evidence가 아니다. +- **Numerical Review questions:** finite-rotation nodal-moment work가 확정되기 전 blocking 가능한가; + exact geometry/mesh/section/load distribution과 analytical quantity projection; full-circle state를 + fixed-step/no-cutback Full Newton으로 안전하게 도달시킬 increment와 tolerance. + +### B-08 — NAFEMS 3DNLG-1 Z-shaped cantilever (`B`) + +- **Exact public candidate artifact:** S8의 `n3g1x33x_s4.inp`와 `n3g1x33x_s4r.inp`. + 페이지는 `t=1.7`, `E=2.0e5`, `nu=0.3`, built-in end, concentrated `P=4000`, `1 x 72` + S4/S4R mesh와 source tables를 명시한다. local stored artifact/CSV는 없음. +- **Target quantities:** load `104.5`, `1263.0`, `4000.0`에서 tip displacement 및 section A moment; + accepted path, root reactions, mesh/source identity. +- **Cannot verify:** curved-shell or distorted-mesh membrane locking, pure rigid objectivity, tangent derivative, + rollback. source S4 result 일치는 formulation/integration/stabilization equivalence를 뜻하지 않는다. +- **Assumptions/limits:** public input의 keyword, node/element orientation, output/moment definition을 FESA + subset과 대조해야 한다. NAFEMS original R0029의 independent-source details는 paywall gap이다. +- **Numerical Review questions:** exact public input을 그대로 지원할 수 있는지 또는 adaptation이 + 필요한지; moment-at-A를 FESA authoritative output에서 동일 quantity/frame으로 얻을 수 있는지; + source table 중 independent target을 식별할 수 있는지; 어떤 quantities가 blocking/warning인지. + +### B-09 — NAFEMS 3DNLG-9 pinched hemisphere (`B`) + +- **Exact public candidate artifact:** S9의 S4 `n3g9xe4x.inp`, S4R `n3g9xf4x.inp`. + page는 `E=6.825e7`, `nu=0.3`, symmetry constraints, diametrical inward/outward point load + `P=100`과 source tables를 제공한다. S16 §3.4/Table 5a는 closely related hemisphere의 + `P/Pmax=0.05..1.00` dense A/B displacement table을 제공한다. local stored artifact/CSV는 없음. +- **Target quantities:** `P=40,60,100`에서 points A/B radial displacement, load–displacement path, + symmetry, reactions와 curved-shell mesh trend. +- **Cannot verify:** independent Abaqus verification—S9 자체가 NAFEMS published values가 Abaqus로 + 얻어졌다고 경고한다—또는 tangent/rollback/pure moment work. +- **Assumptions/limits:** symmetry shorthand, spherical geometry/directors, exact node identity와 radial + projection이 supported subset에 맞아야 한다. original MITC4의 membrane-locking 위험 때문에 + MITC4+ 또는 higher-order 결과 수준을 기대해서는 안 된다. S16 dense values 역시 Abaqus S4R로 + 계산되었으므로 independent-source gap을 닫지 않는다. +- **Numerical Review questions:** R0029의 other-source 결과를 합법적으로 확인할 수 있는지; + exact public deck subset compatibility; regular/distorted/mesh sequence와 target rows; known-locking + limitation을 acceptance와 characterization 중 어디에 둘지. + +### B-10 — Original-MITC4 locking/distortion characterization (`C`) + +- **Exact candidate artifact:** S6 Fig. 14–16의 cylindrical shell bending geometry와 + `a/R=1/100, 1/1000, 1/10000`, regular/distorted `12 x 12` meshes; Fig. 17–20의 hemispherical + shell, regular/distorted `8 x 8`, `12 x 12` meshes. 논문 PDF의 geometry/material/load 설명은 공개다. +- **Artifact gap:** machine-readable inputs/curves가 없고 fine MITC9 reference는 논문 graph뿐이다. + cylindrical case의 distributed edge moment는 현재 input scope와 맞지 않는다. +- **Target quantities:** thickness와 distortion에 따른 displacement-curve trend, rank/conditioning, + original MITC4와 reference curve의 qualitative separation. +- **Cannot verify:** exact blocking reference comparison, FESA MITC4+ behavior, current input-path acceptance. +- **Assumptions/limits:** characterization-only. S6는 original MITC4가 thin distorted cases와 일부 + large-response meshes에서 membrane lock함을 보여 주므로 실패 경향을 숨기지 않는다. +- **Numerical Review questions:** point-load-compatible hemisphere만 optional study로 남길지; graph + digitization을 금지하고 qualitative known limitation으로만 쓸지; performance adequacy의 최소 범위. + +### B-11 — Shell MMS / exact-solution expansion (`C`) + +- **Exact public candidate artifact:** S13의 Figshare source-term notebook와 solid-mechanics examples. +- **Artifact gap:** FESA TL MITC4 shell kinematics에 대한 manufactured midsurface/director field, + compatible nodal CLOAD/BOUNDARY-only source, analytical resultants와 convergence data가 없다. +- **Target quantities:** 향후 shell-specific MMS를 만들 경우 spatial order, residual/source balance, + strain/stress/resultant error norms와 mesh refinement rate. 현재는 B-07M analytical circle을 MES + (method of exact solutions) 후보로 우선한다. +- **Cannot verify:** current feature를 그대로 실행할 수 없음; S13의 3-D body source와 material cases는 + current input/material scope 밖이다. +- **Assumptions/limits:** shell MMS를 위해 distributed/body source 또는 새로운 BC meaning을 추가하면 + approved scope change다. all-boundary prescribed manufactured state는 global nonlinear solve를 충분히 + exercise하지 않는다. +- **Numerical Review questions:** current release에서 MMS를 nonblocking gap으로 둘지; nodal-load-only + admissible exact state를 유도할 수 있는지; spatial convergence study가 acceptance에 필요한지. + +## 6. Verification Relevance + +| evidence class | candidates | 검증하는 것 | 검증하지 못하는 것 | +| --- | --- | --- | --- | +| code verification | B-01, B-02, B-03, B-04, B-05, B-06 | linearization, coordinate map, objectivity/covariance, equilibrium/reaction, state lifecycle, deterministic order | 실제 구조물의 물리 validity 전부 | +| exact/MES comparison | B-07M | large-rotation kinematics, moment work, analytical response path | general curved shell, point force, drilling accuracy | +| solution verification / benchmark comparison | B-07F, B-08, B-09 | assembled nonlinear response, path, curvature, nodal dead load, mesh behavior | 내부 formulation equivalence, tangent consistency, rollback | +| known-limit characterization | B-10 | original MITC4 membrane-locking/distortion sensitivity를 드러냄 | blocking exact target 또는 MITC4+ 성능 | +| MMS method candidate | B-11 | 향후 equation/source implementation과 spatial order | current input scope에서 즉시 실행 가능한 gate | +| reference comparison | Stage-4에서 승인할 stored nonlinear input/CSV | stable source/component mapping과 `docs/TOLERANCE.md` gate | formulation identity, objectivity, state integrity | +| validation | 현재 exact candidate 없음 | — | experimental reality agreement. 이번 release gate를 verification과 validation으로 혼동하지 않음 | + +한 benchmark의 nodal displacement 일치로 전체 기능을 승인해서는 안 된다. 최소 blocking portfolio는 +B-01~B-06의 독립 invariant/software checks와, point-dead-load B-07F 또는 exact subset이 확인된 +B-08/B-09 중 적어도 하나의 large-response problem을 조합하는 방향이 타당하다. O-MOM-01 해소 +후 analytical B-07M을 추가하면 finite-moment work evidence가 강화된다. 이는 +**research recommendation**이며 exact blocking set과 tolerance는 Numerical Review 소유다. + +## 7. Applicability Limits + +| axis | applicable | not established / excluded | +| --- | --- | --- | +| nonlinearity | fixed-reference Total Lagrangian geometric nonlinearity | Updated Lagrangian, corotational, material nonlinearity, finite-strain constitutive validation | +| element | four-node FESA-MITC4 mapping for source S4/S4R; Reissner–Mindlin-type director shell | MITC4+, MITC9, physical drilling/MITC4-D, continuum-shell 또는 Abaqus S4/S4R internal behavior | +| material/section | homogeneous isotropic materially linear shell; user-consistent units | composite, plasticity, hyperelasticity, thickness stretch/material history | +| kinematics | large displacement/finite rotation with small elastic strain applicability | singular/degenerate director interpolation, sharp folds/intersections/hinges without separate evidence | +| loads | proportional fixed-global nodal force and moment; prescribed global targets | follower pressure/force, distributed/body/edge load, non-proportional path, arc-length/control displacement | +| solver path | fixed increments, Full Newton, fresh tangent/solve, no correction modification | modified/quasi-Newton, line search, damping, adaptive growth/cutback/retry, limit-point traversal guarantee | +| integration | source-backed `2x2x2` candidate and existing FESA common S4/S4R convention | source-label-selected Abaqus integration, one-point reduction/hourglass or undocumented selective integration | +| locking | transverse-shear MITC mitigation | general locking-free claim; distorted curved original MITC4 has membrane-locking risk | +| outputs/reference | accepted committed states; exact stable source/component matching after Stage-4 contract | trial HDF5 history, vendor internal variables, inferred units/coordinates, artifact row averaging/normalization | +| verification | analytical/invariant/patch/benchmark/software-failure portfolio | one-value validation claim, automatic Abaqus/Midas equivalence, current linear artifacts as nonlinear reference | + +## 8. Open Issues and Source Disagreements + +| id | type | issue / conflict | downstream acceptance question | +| --- | --- | --- | --- | +| O-ROT-01 | formulation | multiplicative side/frame/retraction, accumulated chart/recentering과 first/second derivative 미정 | Formulation이 하나의 objective state/update convention을 완전 선형화할 수 있는가? | +| O-ROT-02 | formulation/numerical | nodal triad/director의 Gauss/tying interpolation과 normalization derivative 미정 | opposed/degenerate director validation 및 objectivity test가 무엇인가? | +| O-MAP-01 | formulation | nonlinear `24 global -> 20 physical + 4 drill` map과 map Hessian 미정 | complete global residual/tangent가 directional-derivative gate를 통과하는가? | +| O-DRILL-01 | formulation/numerical | objective drilling potential, scale/state dependence와 exact Hessian 미정 | six physical rigid modes를 보존하며 pure drill만 regularize하는가? | +| O-DRILL-02 | formulation/numerical | finite state에서 director-parallel applied moment의 판정과 physical moment/numerical drill 분리 미정 | drilling-direction load가 physical work나 stabilization에 섞이지 않고 결정적으로 거부되는가? | +| O-MOM-01 | formulation | fixed-spatial nodal moment의 multiplicative rotation work/conjugacy 미정 | no-follower 계약을 지키면서 residual/tangent와 B-07M을 정의할 수 있는가? | +| O-BC-01 | formulation/numerical | absolute prescribed finite rotation의 factor path와 constrained correction 좌표 미정 | factor endpoints, intermediate `Q`, reaction work와 rollback identity가 유일한가? | +| O-SYM-01 | numerical | complete tangent symmetry가 conservative internal/drill/moment 선택 후에야 판정 가능 | symmetry를 blocking invariant로 둘지, 어떤 scaled norm을 쓸지? | +| O-REF-01 | reference readiness | exact stored nonlinear `.inp`/CSV가 repository에 없음 | B-08 또는 B-09의 exact deck/rows를 합법적으로 저장·승인할지, 아니면 다른 artifact를 선택할지? | +| O-REF-02 | source access | NAFEMS R0029 full report는 paid/private; 공개 Abaqus 3DNLG-9 값은 독립 NAFEMS evidence가 아님 | independent target/provenance를 추가 확보할 수 있는가? 확보 못하면 claim을 어떻게 제한할지? | +| O-TOL-01 | numerical | tangent, objectivity, `Q` invariant, balance, symmetry, endpoint arithmetic tolerance 미정 | scale-aware case-specific gate를 Stage-4 전에 모두 고정할 수 있는가? | +| O-BENCH-01 | scope/numerical | B-07F는 exact deck 부재/vendor-result 경계, B-07M은 nodal moment work, B-09는 curved locking/subset, B-08은 moment output identity gap이 있음 | large-response blocking benchmark를 어떤 exact artifact/quantity로 선택할지? | +| O-STEP-01 | numerical | no-cutback Full Newton이 published benchmark load intervals에서 수렴한다는 evidence 없음 | fixed increment를 benchmark마다 어떻게 정하고, deterministic nonconvergence와 formulation failure를 구분할지? | +| O-MMS-01 | method | public MMS artifact는 3-D solid/body-source이고 shell/CLOAD subset과 불일치 | first release에서 nonblocking으로 남길지, scope-preserving exact nodal-load case가 가능한지? | + +명시적 source disagreement/비교 경계는 다음과 같다. + +1. S1/S6의 nonlinear shell은 node당 five physical DOFs를 쓰지만 P1은 six global DOFs와 + numerical drill을 요구한다. 이 차이는 구현 detail이 아니라 O-MAP-01/O-DRILL-01의 정식화 gap이다. +2. S6의 MITC4+는 membrane assumed strain을 추가하고 original MITC4보다 distorted nonlinear + mesh에서 더 좋은 결과를 보인다. FESA는 original-style MITC4이므로 그 성능을 상속하지 않는다. +3. Abaqus S4와 S4R의 공개 결과/inputs는 benchmark evidence 후보지만 FESA source mapping과 + Abaqus integration, stabilization, rotation 또는 output recovery의 동일성을 뜻하지 않는다. +4. S7의 Abaqus production algorithm에는 adaptive cutback 등 P1이 의도적으로 제외한 control이 + 있다. Newton의 일반 same-state Jacobian evidence만 사용하며 runtime-control 동등성을 주장하지 않는다. + +## 9. Downstream Handoff + +### 9.1 Formulation Agent에 전달할 evidence와 미결정 + +1. S1/S6을 출발점으로 fixed-initial-reference TL shell의 kinematic/virtual-work 계통을 다시 + 유도하되, materially linear law와 existing physical MITC shear/`2x2x2` boundary만 보존한다. +2. S2–S5를 근거로 committed/trial `Q`, director, chosen multiplicative retraction, interpolation, + first/second variation을 하나의 objective/path-defined convention으로 제시한다. +3. O-MAP-01의 exact global 24-DOF residual/tangent와 state-dependent map Hessian을 완성한다. + `docs/linear-static-mitc4-shell/formulation.md` §15는 gap inventory로만 사용한다. +4. O-DRILL-01/O-DRILL-02의 objective numerical drilling potential과 exact residual/Hessian, + physical recovery separation, rigid-mode preservation을 정의한다. physical drilling 모델로 scope를 + 바꾸지 않는다. +5. fixed-global force와 moment의 external virtual work, O-MOM-01 nodal-moment conjugacy/derivative, + O-BC-01 prescribed finite-rotation path와 constrained correction을 명시한다. +6. same-trial complete residual과 algorithmic tangent에 material/geometric/map/drill/load-work terms가 + 빠짐없이 대응함을 trace한다. 이 연구의 benchmark formula를 FESA governing equation으로 복사하지 않는다. + +### 9.2 Numerical Review Agent에 전달할 benchmark/reference evidence + +1. B-01~B-06을 각기 독립 blocking 후보로 검토하고, quantities, norms, scales, perturbation study, + invariant/balance/rollback tolerance를 `O-TOL-01` 해소와 함께 고정한다. +2. B-07F는 O-MOM-01과 독립인 point-dead-load large-rotation 후보로 먼저 검토하되 S16의 + vendor S4R values를 independent/formulation-equivalent target으로 부르지 않는다. B-07M + pure-moment MES는 O-MOM-01이 해결된 뒤에만 blocking 여부를 정하고, analytical equation, + mesh/section/load distribution과 target projection을 별도로 재현·검토한다. +3. public exact filenames가 있는 B-08 `n3g1x33x_s4.inp`/`_s4r.inp`와 B-09 + `n3g9xe4x.inp`/`n3g9xf4x.inp`의 keyword subset, stable identities, units/coordinates, target row + definitions와 provenance를 검사한다. 이 단계에서는 실행·생성·rename하지 않는다. +4. `reference/shell/`와 `reference/shellR/`는 `nlgeom=NO` linear artifacts다. B-01 baseline 이상의 + nonlinear-readiness를 부여하지 말고 O-REF-01을 exact stored nonlinear artifact gap으로 유지한다. +5. B-10은 original MITC4 known-limit characterization으로 분류하고 MITC4+ curves를 FESA target으로 + 쓰지 않는다. B-11 MMS는 current scope compatibility가 입증되지 않으면 nonblocking gap이다. +6. selected external reference만 stable row identity와 `docs/TOLERANCE.md` family-scale policy로 + 비교한다. missing/extra/duplicate/nonfinite precheck와 blocking/warning family를 artifact별로 정한다. +7. fixed increment/no-cutback 조건에서 benchmark가 실제로 traversable한지 O-STEP-01을 먼저 판정한다. + convergence failure를 임의 tolerance 완화나 hidden retry로 숨기지 않는다. + +### 9.3 Coordinator에 반환하는 gate 의미 + +- Research quality gate는 통과한다: approved gaps에 직접 대응하는 Tier 1/2 evidence, applicability + limits, exact public/local candidate identities, artifact gaps와 downstream acceptance questions가 있다. +- 이 `passed`는 formulation 또는 nonlinear reference readiness 통과를 뜻하지 않는다. + O-ROT/O-MAP/O-DRILL/O-MOM/O-BC는 Formulation gate, O-TOL/O-REF/O-BENCH/O-STEP은 Numerical + Review gate에서 해소해야 한다. +- requirements, code, tests, CMake, I/O, phase 또는 reference artifact는 이 stage에서 변경하지 않는다. + +## 10. Self-Audit and Research Quality Gate + +| audit item | result | evidence | +| --- | --- | --- | +| approved requirement trace | pass | RQ와 Sections 4–9가 NSNR-003/041/074/006/048/018/063/011/019/030/034를 직접 다룸 | +| key theory claim sourcing | pass | TL/MITC4 S1/S6, rotations S2–S5, Newton S7, V&V/MMS S11–S13, tabulated benchmark evidence S16 | +| fact/decision/inference/open separation | pass | Section 4의 각 claim label과 Section 8 gap IDs | +| benchmark exactness | pass | B-01~B-06, B-07F/B-07M, B-08~B-11마다 exact artifact 또는 explicit artifact gap, target, cannot-verify, limit, Numerical Review question 기재 | +| nonlinear artifact honesty | pass | P6/B-01에서 `reference/shell*`의 `nlgeom=NO`와 nonlinear gap을 명시 | +| compatibility restraint | pass | S4/S4R/MITC4+ 및 Abaqus/NAFEMS 경계를 Sections 3, 7, 8에 명시; internal equivalence claim 없음 | +| tolerance restraint | pass | source가 공개한 benchmark load/geometry만 후보로 기록; 새로운 reference/invariant tolerance를 만들지 않음 | +| source access/licensing limits | pass | NAFEMS/ASME paywall, publisher access, public author copy/CC BY와 graph-only limits 기록 | +| downstream sufficiency | pass | exact formulation and Numerical Review action lists와 owner별 open issue 제공 | +| ownership | pass | 이 artifact만 Research Agent 소유; external solver/reference 실행·변경 없음 | + +검색했지만 확보하지 못한 핵심 evidence는 (1) 공개·독립·machine-readable NAFEMS R0029 target +source, (2) FESA subset에 이미 맞는 stored nonlinear S4/S4R input/CSV, (3) original FESA-MITC4의 +objective 24-DOF drilling/finite nodal-moment 정식화다. 이 부재를 source compatibility 주장이나 +새 numerical value로 메우지 않았다. diff --git a/reference/shell/shell stresses.csv b/reference/shell/shell stresses.csv index 26d95de..6a845e1 100644 --- a/reference/shell/shell stresses.csv +++ b/reference/shell/shell stresses.csv @@ -1,289 +1,289 @@ -Part Instance Name, Element Label, Node Label, S-S11, S-S22, S-S33, S-S12 -PART-1-1,1,1,5.842455470E+04,1.947485000E+05,0.000000000E+00,1.220703120E-04 -PART-1-1,30,1,5.842455470E+04,1.947485000E+05,0.000000000E+00,1.220703120E-04 -PART-1-1,30,1,-5.842455470E+04,-1.947485000E+05,0.000000000E+00,-1.220703120E-04 -PART-1-1,1,1,-5.842455470E+04,-1.947485000E+05,0.000000000E+00,-1.220703120E-04 -PART-1-1,28,2,-3.423266250E+05,-3.423266250E+05,0.000000000E+00,2.441406250E-04 -PART-1-1,28,2,3.423266250E+05,3.423266250E+05,0.000000000E+00,-2.441406250E-04 -PART-1-1,19,2,-3.423266250E+05,-3.423266250E+05,0.000000000E+00,2.441406250E-04 -PART-1-1,19,2,3.423266250E+05,3.423266250E+05,0.000000000E+00,-2.441406250E-04 -PART-1-1,12,2,-3.423266250E+05,-3.423266250E+05,0.000000000E+00,2.441406250E-04 -PART-1-1,12,2,3.423266250E+05,3.423266250E+05,0.000000000E+00,-2.441406250E-04 -PART-1-1,3,2,-3.423266250E+05,-3.423266250E+05,0.000000000E+00,2.441406250E-04 -PART-1-1,3,2,3.423266250E+05,3.423266250E+05,0.000000000E+00,-2.441406250E-04 -PART-1-1,25,3,1.947485000E+05,5.842455470E+04,0.000000000E+00,0.000000000E+00 -PART-1-1,9,3,-1.947485000E+05,-5.842455470E+04,0.000000000E+00,0.000000000E+00 -PART-1-1,9,3,1.947485000E+05,5.842455470E+04,0.000000000E+00,0.000000000E+00 -PART-1-1,25,3,-1.947485000E+05,-5.842455470E+04,0.000000000E+00,0.000000000E+00 -PART-1-1,7,4,0.000000000E+00,0.000000000E+00,0.000000000E+00,1.953125000E-03 -PART-1-1,7,4,0.000000000E+00,0.000000000E+00,0.000000000E+00,-1.953125000E-03 -PART-1-1,21,5,5.842455470E+04,1.947485000E+05,0.000000000E+00,1.220703120E-04 -PART-1-1,10,5,5.842455470E+04,1.947485000E+05,0.000000000E+00,1.220703120E-04 -PART-1-1,10,5,-5.842455470E+04,-1.947485000E+05,0.000000000E+00,-1.220703120E-04 -PART-1-1,21,5,-5.842455470E+04,-1.947485000E+05,0.000000000E+00,-1.220703120E-04 -PART-1-1,18,6,-1.947485000E+05,-5.842455470E+04,0.000000000E+00,0.000000000E+00 -PART-1-1,34,6,-1.947485000E+05,-5.842455470E+04,0.000000000E+00,0.000000000E+00 -PART-1-1,18,6,1.947485000E+05,5.842455470E+04,0.000000000E+00,0.000000000E+00 -PART-1-1,34,6,1.947485000E+05,5.842455470E+04,0.000000000E+00,0.000000000E+00 -PART-1-1,16,7,0.000000000E+00,0.000000000E+00,0.000000000E+00,1.953125000E-03 -PART-1-1,16,7,0.000000000E+00,0.000000000E+00,0.000000000E+00,-1.953125000E-03 -PART-1-1,27,8,0.000000000E+00,0.000000000E+00,0.000000000E+00,-1.953125000E-03 -PART-1-1,27,8,0.000000000E+00,0.000000000E+00,0.000000000E+00,1.953125000E-03 -PART-1-1,36,9,0.000000000E+00,0.000000000E+00,0.000000000E+00,1.953125000E-03 -PART-1-1,36,9,0.000000000E+00,0.000000000E+00,0.000000000E+00,-1.953125000E-03 -PART-1-1,1,10,1.129313870E+04,-1.164263670E+05,0.000000000E+00,2.441406250E-04 -PART-1-1,1,10,-1.129313870E+04,1.164263670E+05,0.000000000E+00,-2.441406250E-04 -PART-1-1,30,10,1.129313870E+04,-1.164263670E+05,0.000000000E+00,2.441406250E-04 -PART-1-1,29,10,1.129313870E+04,-1.164263670E+05,0.000000000E+00,2.441406250E-04 -PART-1-1,2,10,1.129313870E+04,-1.164263670E+05,0.000000000E+00,2.441406250E-04 -PART-1-1,2,10,-1.129313870E+04,1.164263670E+05,0.000000000E+00,-2.441406250E-04 -PART-1-1,30,10,-1.129313870E+04,1.164263670E+05,0.000000000E+00,-2.441406250E-04 -PART-1-1,29,10,-1.129313870E+04,1.164263670E+05,0.000000000E+00,-2.441406250E-04 -PART-1-1,3,11,1.922575620E+05,1.462878280E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,28,11,-1.922575620E+05,-1.462878280E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,2,11,-1.922575620E+05,-1.462878280E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,2,11,1.922575620E+05,1.462878280E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,28,11,1.922575620E+05,1.462878280E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,3,11,-1.922575620E+05,-1.462878280E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,29,11,1.922575620E+05,1.462878280E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,29,11,-1.922575620E+05,-1.462878280E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,19,12,1.462878120E+05,1.922575620E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,3,12,1.462878120E+05,1.922575620E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,3,12,-1.462878120E+05,-1.922575620E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,22,12,1.462878120E+05,1.922575620E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,6,12,1.462878120E+05,1.922575620E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,6,12,-1.462878120E+05,-1.922575620E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,19,12,-1.462878120E+05,-1.922575620E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,22,12,-1.462878120E+05,-1.922575620E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,25,13,1.164263670E+05,-1.129313870E+04,0.000000000E+00,-4.882812500E-04 -PART-1-1,25,13,-1.164263670E+05,1.129313870E+04,0.000000000E+00,4.882812500E-04 -PART-1-1,22,13,1.164263670E+05,-1.129313870E+04,0.000000000E+00,-4.882812500E-04 -PART-1-1,22,13,-1.164263670E+05,1.129313870E+04,0.000000000E+00,4.882812500E-04 -PART-1-1,9,13,-1.164263670E+05,1.129313870E+04,0.000000000E+00,4.882812500E-04 -PART-1-1,6,13,1.164263670E+05,-1.129313870E+04,0.000000000E+00,-4.882812500E-04 -PART-1-1,9,13,1.164263670E+05,-1.129313870E+04,0.000000000E+00,-4.882812500E-04 -PART-1-1,6,13,-1.164263670E+05,1.129313870E+04,0.000000000E+00,4.882812500E-04 -PART-1-1,8,14,1.582039380E+05,4.746118750E+04,0.000000000E+00,1.777732620E+04 -PART-1-1,8,14,-1.582039380E+05,-4.746118750E+04,0.000000000E+00,-1.777732620E+04 -PART-1-1,9,14,1.582039380E+05,4.746118750E+04,0.000000000E+00,1.777732620E+04 -PART-1-1,9,14,-1.582039380E+05,-4.746118750E+04,0.000000000E+00,-1.777732620E+04 -PART-1-1,7,15,-5.956113280E+04,-1.786834180E+04,0.000000000E+00,-2.084639450E+04 -PART-1-1,8,15,5.956113280E+04,1.786834180E+04,0.000000000E+00,2.084639450E+04 -PART-1-1,8,15,-5.956113280E+04,-1.786834180E+04,0.000000000E+00,-2.084639450E+04 -PART-1-1,7,15,5.956113280E+04,1.786834180E+04,0.000000000E+00,2.084639450E+04 -PART-1-1,7,16,1.786834180E+04,5.956113280E+04,0.000000000E+00,2.084639450E+04 -PART-1-1,4,16,1.786834180E+04,5.956113280E+04,0.000000000E+00,2.084639450E+04 -PART-1-1,7,16,-1.786834180E+04,-5.956113280E+04,0.000000000E+00,-2.084639450E+04 -PART-1-1,4,16,-1.786834180E+04,-5.956113280E+04,0.000000000E+00,-2.084639450E+04 -PART-1-1,4,17,-4.746118750E+04,-1.582039530E+05,0.000000000E+00,-1.777732810E+04 -PART-1-1,4,17,4.746118750E+04,1.582039530E+05,0.000000000E+00,1.777732810E+04 -PART-1-1,1,17,4.746118750E+04,1.582039530E+05,0.000000000E+00,1.777732810E+04 -PART-1-1,1,17,-4.746118750E+04,-1.582039530E+05,0.000000000E+00,-1.777732810E+04 -PART-1-1,11,18,-1.129313870E+04,1.164263670E+05,0.000000000E+00,-2.441406250E-04 -PART-1-1,10,18,-1.129313870E+04,1.164263670E+05,0.000000000E+00,-2.441406250E-04 -PART-1-1,10,18,1.129313870E+04,-1.164263670E+05,0.000000000E+00,2.441406250E-04 -PART-1-1,21,18,-1.129313870E+04,1.164263670E+05,0.000000000E+00,-2.441406250E-04 -PART-1-1,20,18,1.129313870E+04,-1.164263670E+05,0.000000000E+00,2.441406250E-04 -PART-1-1,21,18,1.129313870E+04,-1.164263670E+05,0.000000000E+00,2.441406250E-04 -PART-1-1,11,18,1.129313870E+04,-1.164263670E+05,0.000000000E+00,2.441406250E-04 -PART-1-1,20,18,-1.129313870E+04,1.164263670E+05,0.000000000E+00,-2.441406250E-04 -PART-1-1,12,19,1.922575620E+05,1.462878280E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,12,19,-1.922575620E+05,-1.462878280E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,20,19,-1.922575620E+05,-1.462878280E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,20,19,1.922575620E+05,1.462878280E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,11,19,1.922575620E+05,1.462878280E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,19,19,1.922575620E+05,1.462878280E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,19,19,-1.922575620E+05,-1.462878280E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,11,19,-1.922575620E+05,-1.462878280E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,12,20,-1.462878120E+05,-1.922575620E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,31,20,-1.462878120E+05,-1.922575620E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,28,20,-1.462878120E+05,-1.922575620E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,15,20,1.462878120E+05,1.922575620E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,15,20,-1.462878120E+05,-1.922575620E+05,0.000000000E+00,9.765625000E-04 -PART-1-1,28,20,1.462878120E+05,1.922575620E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,12,20,1.462878120E+05,1.922575620E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,31,20,1.462878120E+05,1.922575620E+05,0.000000000E+00,-9.765625000E-04 -PART-1-1,15,21,1.164263670E+05,-1.129313870E+04,0.000000000E+00,-4.882812500E-04 -PART-1-1,15,21,-1.164263670E+05,1.129313870E+04,0.000000000E+00,4.882812500E-04 -PART-1-1,34,21,1.164263670E+05,-1.129313870E+04,0.000000000E+00,-4.882812500E-04 -PART-1-1,18,21,-1.164263670E+05,1.129313870E+04,0.000000000E+00,4.882812500E-04 -PART-1-1,18,21,1.164263670E+05,-1.129313870E+04,0.000000000E+00,-4.882812500E-04 -PART-1-1,31,21,-1.164263670E+05,1.129313870E+04,0.000000000E+00,4.882812500E-04 -PART-1-1,31,21,1.164263670E+05,-1.129313870E+04,0.000000000E+00,-4.882812500E-04 -PART-1-1,34,21,-1.164263670E+05,1.129313870E+04,0.000000000E+00,4.882812500E-04 -PART-1-1,18,22,1.582039380E+05,4.746118750E+04,0.000000000E+00,1.777732620E+04 -PART-1-1,18,22,-1.582039380E+05,-4.746118750E+04,0.000000000E+00,-1.777732620E+04 -PART-1-1,17,22,1.582039380E+05,4.746118750E+04,0.000000000E+00,1.777732620E+04 -PART-1-1,17,22,-1.582039380E+05,-4.746118750E+04,0.000000000E+00,-1.777732620E+04 -PART-1-1,17,23,5.956113280E+04,1.786834180E+04,0.000000000E+00,2.084639450E+04 -PART-1-1,17,23,-5.956113280E+04,-1.786834180E+04,0.000000000E+00,-2.084639450E+04 -PART-1-1,16,23,5.956113280E+04,1.786834180E+04,0.000000000E+00,2.084639450E+04 -PART-1-1,16,23,-5.956113280E+04,-1.786834180E+04,0.000000000E+00,-2.084639450E+04 -PART-1-1,13,24,-1.786834180E+04,-5.956113280E+04,0.000000000E+00,-2.084639450E+04 -PART-1-1,16,24,-1.786834180E+04,-5.956113280E+04,0.000000000E+00,-2.084639450E+04 -PART-1-1,16,24,1.786834180E+04,5.956113280E+04,0.000000000E+00,2.084639450E+04 -PART-1-1,13,24,1.786834180E+04,5.956113280E+04,0.000000000E+00,2.084639450E+04 -PART-1-1,13,25,4.746118750E+04,1.582039530E+05,0.000000000E+00,1.777732810E+04 -PART-1-1,10,25,-4.746118750E+04,-1.582039530E+05,0.000000000E+00,-1.777732810E+04 -PART-1-1,13,25,-4.746118750E+04,-1.582039530E+05,0.000000000E+00,-1.777732810E+04 -PART-1-1,10,25,4.746118750E+04,1.582039530E+05,0.000000000E+00,1.777732810E+04 -PART-1-1,24,26,-4.746118750E+04,-1.582039380E+05,0.000000000E+00,1.777732810E+04 -PART-1-1,21,26,4.746118750E+04,1.582039380E+05,0.000000000E+00,-1.777732810E+04 -PART-1-1,21,26,-4.746118750E+04,-1.582039380E+05,0.000000000E+00,1.777732810E+04 -PART-1-1,24,26,4.746118750E+04,1.582039380E+05,0.000000000E+00,-1.777732810E+04 -PART-1-1,27,27,-1.786834180E+04,-5.956113280E+04,0.000000000E+00,2.084639450E+04 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MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301503120E+04,-3.301503120E+04,0.000000000E+00,5.537139060E+04 +PART-1-1,36,49,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301503120E+04,3.301503120E+04,0.000000000E+00,-5.537139060E+04 diff --git a/reference/shellNL/shellNL displacements.csv b/reference/shellNL/shellNL displacements.csv new file mode 100644 index 0000000..0d80e02 --- /dev/null +++ b/reference/shellNL/shellNL displacements.csv @@ -0,0 +1,50 @@ +Frame,Part Instance Name, Node Label, U-U1, U-U2, U-U3, UR-UR1, UR-UR2, UR-UR3 +Increment 10: Step Time = 1.000,PART-1-1,1,2.188126210E-37,9.534856260E-37,-5.888490180E-33,-5.374006350E-32,8.671701910E-33,-1.594921620E-38 +Increment 10: Step Time = 1.000,PART-1-1,2,-3.424411360E-22,1.492887960E-22,-2.374082030E-05,-7.875144140E-22,2.028240650E-22,-1.149104880E-16 +Increment 10: Step Time = 1.000,PART-1-1,3,9.535853540E-37,2.187793030E-37,-5.888490180E-33,-8.671701910E-33,5.374006350E-32,1.594560640E-38 +Increment 10: Step Time = 1.000,PART-1-1,4,1.062323950E-38,1.061095850E-38,-5.745323700E-44,2.326155450E-43,-2.326155450E-43,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,5,-2.188126210E-37,-9.534856260E-37,-5.888490180E-33,5.374006350E-32,-8.671701910E-33,-1.594921620E-38 +Increment 10: Step Time = 1.000,PART-1-1,6,-9.535853540E-37,-2.187793030E-37,-5.888490180E-33,8.671701910E-33,-5.374006350E-32,1.594560640E-38 +Increment 10: Step Time = 1.000,PART-1-1,7,-1.062323950E-38,-1.061095850E-38,-5.745323700E-44,-2.326155450E-43,2.326155450E-43,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,8,1.062266630E-38,-1.062298160E-38,-5.745323700E-44,-2.326155450E-43,-2.326155450E-43,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,9,-1.062266630E-38,1.062298160E-38,-5.745323700E-44,2.326155450E-43,2.326155450E-43,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,10,3.474719200E-16,1.293161410E-11,-5.102237540E-06,-5.626068290E-06,-2.931340880E-21,1.443065280E-18 +Increment 10: Step Time = 1.000,PART-1-1,11,-1.726116560E-16,-2.861629990E-12,-1.615657860E-05,-7.607257430E-06,2.311731110E-21,1.197342750E-16 +Increment 10: Step Time = 1.000,PART-1-1,12,-2.862247550E-12,2.104234190E-16,-1.615657860E-05,-8.289949670E-22,7.607257430E-06,-2.532911570E-17 +Increment 10: Step Time = 1.000,PART-1-1,13,1.293132790E-11,-3.742547580E-16,-5.102237540E-06,-2.244465530E-21,5.626068290E-06,-8.173356410E-17 +Increment 10: Step Time = 1.000,PART-1-1,14,8.146328670E-37,2.214433850E-37,-3.862132240E-33,-6.214571210E-33,5.544442450E-32,8.122889990E-39 +Increment 10: Step Time = 1.000,PART-1-1,15,3.634199410E-37,1.481777840E-37,-3.437612470E-34,-8.176467610E-33,2.944981870E-32,5.496142010E-39 +Increment 10: Step Time = 1.000,PART-1-1,16,-7.869300370E-38,1.742082370E-37,4.147901210E-36,-5.905084850E-33,-9.006172110E-34,-5.283594460E-39 +Increment 10: Step Time = 1.000,PART-1-1,17,-1.479949420E-37,4.792022820E-37,-2.420134220E-33,-2.430273740E-32,-3.378631580E-33,3.810077280E-39 +Increment 10: Step Time = 1.000,PART-1-1,18,-3.474720260E-16,-1.293161410E-11,-5.102237540E-06,5.626068290E-06,2.810486080E-21,1.443040570E-18 +Increment 10: Step Time = 1.000,PART-1-1,19,1.726114710E-16,2.861629990E-12,-1.615657860E-05,7.607257430E-06,-1.391752080E-21,1.197341820E-16 +Increment 10: Step Time = 1.000,PART-1-1,20,2.862247550E-12,-2.104233920E-16,-1.615657860E-05,-1.940186480E-22,-7.607257430E-06,-2.532916040E-17 +Increment 10: Step Time = 1.000,PART-1-1,21,-1.293132790E-11,3.742547580E-16,-5.102237540E-06,1.972326950E-21,-5.626068290E-06,-8.173357070E-17 +Increment 10: Step Time = 1.000,PART-1-1,22,-8.146328670E-37,-2.214433850E-37,-3.862132240E-33,6.214571210E-33,-5.544442450E-32,8.122889990E-39 +Increment 10: Step Time = 1.000,PART-1-1,23,-3.634199410E-37,-1.481777840E-37,-3.437612470E-34,8.176467610E-33,-2.944981870E-32,5.496142010E-39 +Increment 10: Step Time = 1.000,PART-1-1,24,7.869300370E-38,-1.742082370E-37,4.147901210E-36,5.905084850E-33,9.006172110E-34,-5.283594460E-39 +Increment 10: Step Time = 1.000,PART-1-1,25,1.479949420E-37,-4.792022820E-37,-2.420134220E-33,2.430273740E-32,3.378631580E-33,3.810077280E-39 +Increment 10: Step Time = 1.000,PART-1-1,26,-1.479506160E-37,-4.791990990E-37,-2.420134220E-33,2.430273740E-32,-3.378631580E-33,-3.811062390E-39 +Increment 10: Step Time = 1.000,PART-1-1,27,-7.868808240E-38,-1.742969890E-37,4.147901210E-36,5.905084850E-33,-9.006172110E-34,5.284864030E-39 +Increment 10: Step Time = 1.000,PART-1-1,28,1.742451080E-37,7.874333840E-38,4.147901210E-36,-9.006172110E-34,5.905084850E-33,-5.278797810E-39 +Increment 10: Step Time = 1.000,PART-1-1,29,4.792355100E-37,1.479843930E-37,-2.420134220E-33,-3.378631580E-33,2.430273740E-32,3.807350350E-39 +Increment 10: Step Time = 1.000,PART-1-1,30,1.479506160E-37,4.791990990E-37,-2.420134220E-33,-2.430273740E-32,3.378631580E-33,-3.811062390E-39 +Increment 10: Step Time = 1.000,PART-1-1,31,7.868808240E-38,1.742969890E-37,4.147901210E-36,-5.905084850E-33,9.006172110E-34,5.284864030E-39 +Increment 10: Step Time = 1.000,PART-1-1,32,-1.742451080E-37,-7.874333840E-38,4.147901210E-36,9.006172110E-34,-5.905084850E-33,-5.278797810E-39 +Increment 10: Step Time = 1.000,PART-1-1,33,-4.792355100E-37,-1.479843930E-37,-2.420134220E-33,3.378631580E-33,-2.430273740E-32,3.807350350E-39 +Increment 10: Step Time = 1.000,PART-1-1,34,3.081383890E-12,6.508823860E-12,-3.974393620E-06,-4.570336390E-06,1.467334870E-06,3.177270510E-12 +Increment 10: Step Time = 1.000,PART-1-1,35,-2.225679490E-12,-2.225569340E-12,-1.219086790E-05,-4.710196210E-06,4.710196210E-06,1.743015530E-16 +Increment 10: Step Time = 1.000,PART-1-1,36,2.972663780E-12,2.971908740E-12,-1.432399700E-06,-1.720654950E-06,1.720654950E-06,1.102082510E-16 +Increment 10: Step Time = 1.000,PART-1-1,37,6.507956070E-12,3.080830080E-12,-3.974393620E-06,-1.467334870E-06,4.570336390E-06,-3.177153200E-12 +Increment 10: Step Time = 1.000,PART-1-1,38,-3.081383890E-12,-6.508823860E-12,-3.974393620E-06,4.570336390E-06,-1.467334870E-06,3.177270510E-12 +Increment 10: Step Time = 1.000,PART-1-1,39,2.225679490E-12,2.225569340E-12,-1.219086790E-05,4.710196210E-06,-4.710196210E-06,1.743015530E-16 +Increment 10: Step Time = 1.000,PART-1-1,40,-2.972663780E-12,-2.971908740E-12,-1.432399700E-06,1.720654950E-06,-1.720654950E-06,1.102082440E-16 +Increment 10: Step Time = 1.000,PART-1-1,41,-6.507956070E-12,-3.080830080E-12,-3.974393620E-06,1.467334870E-06,-4.570336390E-06,-3.177153200E-12 +Increment 10: Step Time = 1.000,PART-1-1,42,-2.225000130E-12,2.225258390E-12,-1.219086790E-05,4.710196210E-06,4.710196210E-06,-3.872236930E-17 +Increment 10: Step Time = 1.000,PART-1-1,43,3.081102650E-12,-6.508646050E-12,-3.974393620E-06,4.570336390E-06,1.467334870E-06,-3.177290030E-12 +Increment 10: Step Time = 1.000,PART-1-1,44,6.509021620E-12,-3.081479950E-12,-3.974393620E-06,1.467334870E-06,4.570336390E-06,3.177015940E-12 +Increment 10: Step Time = 1.000,PART-1-1,45,2.972907290E-12,-2.971156740E-12,-1.432399700E-06,1.720654950E-06,1.720654950E-06,2.753750600E-17 +Increment 10: Step Time = 1.000,PART-1-1,46,2.225000130E-12,-2.225258390E-12,-1.219086790E-05,-4.710196210E-06,-4.710196210E-06,-3.872236930E-17 +Increment 10: Step Time = 1.000,PART-1-1,47,-3.081102650E-12,6.508646050E-12,-3.974393620E-06,-4.570336390E-06,-1.467334870E-06,-3.177290030E-12 +Increment 10: Step Time = 1.000,PART-1-1,48,-6.509021620E-12,3.081479950E-12,-3.974393620E-06,-1.467334870E-06,-4.570336390E-06,3.177015940E-12 +Increment 10: Step Time = 1.000,PART-1-1,49,-2.972907290E-12,2.971156740E-12,-1.432399700E-06,-1.720654950E-06,-1.720654950E-06,2.753751100E-17 diff --git a/reference/shellNL/shellNL reactions.csv b/reference/shellNL/shellNL reactions.csv new file mode 100644 index 0000000..866bed1 --- /dev/null +++ b/reference/shellNL/shellNL reactions.csv @@ -0,0 +1,50 @@ +Frame,Part Instance Name, Node Label, RF-RF1, RF-RF2, RF-RF3, RM-RM1, RM-RM2, RM-RM3 +Increment 10: Step Time = 1.000,PART-1-1,1,-5.232752760E-06,-1.916590210E+00,1.177698050E+04,1.954184180E+04,-9.094947020E-13,4.615960170E-07 +Increment 10: Step Time = 1.000,PART-1-1,2,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,3,-1.916631820E+00,-2.101437890E-05,1.177698050E+04,-2.955857780E-12,-1.954184180E+04,4.971754490E-07 +Increment 10: Step Time = 1.000,PART-1-1,4,-9.471606460E-02,-9.471402320E-02,-2.073950580E+01,1.594132080E+03,-1.594132080E+03,9.451013090E-19 +Increment 10: Step Time = 1.000,PART-1-1,5,5.232753210E-06,1.916590210E+00,1.177698050E+04,-1.954184180E+04,1.250555210E-11,4.615961590E-07 +Increment 10: Step Time = 1.000,PART-1-1,6,1.916631820E+00,2.101437710E-05,1.177698050E+04,6.139089240E-12,1.954184180E+04,4.971754490E-07 +Increment 10: Step Time = 1.000,PART-1-1,7,9.471606460E-02,9.471402320E-02,-2.073950580E+01,-1.594132080E+03,1.594132080E+03,1.053521530E-18 +Increment 10: Step Time = 1.000,PART-1-1,8,-9.472383560E-02,9.475927800E-02,-2.073950580E+01,-1.594132080E+03,-1.594132080E+03,-6.776825030E-19 +Increment 10: Step Time = 1.000,PART-1-1,9,9.472383560E-02,-9.475927800E-02,-2.073950580E+01,1.594132080E+03,1.594132080E+03,-6.743083810E-19 +Increment 10: Step Time = 1.000,PART-1-1,10,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,11,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,12,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,13,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,14,-1.292096260E+00,-7.747494430E-02,6.282266110E+03,5.156254270E+02,-1.449948340E+04,-1.273409110E-03 +Increment 10: Step Time = 1.000,PART-1-1,15,-5.106337670E-01,-4.954520240E-02,3.396133420E+02,1.322881960E+03,-6.428164550E+03,-2.987184560E-03 +Increment 10: Step Time = 1.000,PART-1-1,16,-4.952526470E-02,-5.106006860E-01,3.396133420E+02,6.428164550E+03,-1.322881960E+03,2.988364310E-03 +Increment 10: Step Time = 1.000,PART-1-1,17,-7.749996330E-02,-1.292100550E+00,6.282266110E+03,1.449948340E+04,-5.156254270E+02,1.273998990E-03 +Increment 10: Step Time = 1.000,PART-1-1,18,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,19,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,20,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,21,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,22,1.292096260E+00,7.747494430E-02,6.282266110E+03,-5.156254270E+02,1.449948340E+04,-1.273409110E-03 +Increment 10: Step Time = 1.000,PART-1-1,23,5.106337670E-01,4.954520240E-02,3.396133420E+02,-1.322881960E+03,6.428164550E+03,-2.987184560E-03 +Increment 10: Step Time = 1.000,PART-1-1,24,4.952526470E-02,5.106006860E-01,3.396133420E+02,-6.428164550E+03,1.322881960E+03,2.988364310E-03 +Increment 10: Step Time = 1.000,PART-1-1,25,7.749996330E-02,1.292100550E+00,6.282266110E+03,-1.449948340E+04,5.156254270E+02,1.273998990E-03 +Increment 10: Step Time = 1.000,PART-1-1,26,-7.753752920E-02,1.292116640E+00,6.282266110E+03,-1.449948340E+04,-5.156254270E+02,-1.273704110E-03 +Increment 10: Step Time = 1.000,PART-1-1,27,-4.947229850E-02,5.106329920E-01,3.396133420E+02,-6.428164550E+03,-1.322881960E+03,-2.988364310E-03 +Increment 10: Step Time = 1.000,PART-1-1,28,-5.106223230E-01,4.947446290E-02,3.396133420E+02,-1.322881960E+03,-6.428164550E+03,2.986004580E-03 +Increment 10: Step Time = 1.000,PART-1-1,29,-1.292139170E+00,7.751832160E-02,6.282266110E+03,-5.156254270E+02,-1.449948340E+04,1.274293990E-03 +Increment 10: Step Time = 1.000,PART-1-1,30,7.753752920E-02,-1.292116640E+00,6.282266110E+03,1.449948340E+04,5.156254270E+02,-1.273704110E-03 +Increment 10: Step Time = 1.000,PART-1-1,31,4.947229850E-02,-5.106329920E-01,3.396133420E+02,6.428164550E+03,1.322881960E+03,-2.988364310E-03 +Increment 10: Step Time = 1.000,PART-1-1,32,5.106223230E-01,-4.947446290E-02,3.396133420E+02,1.322881960E+03,6.428164550E+03,2.986004580E-03 +Increment 10: Step Time = 1.000,PART-1-1,33,1.292139170E+00,-7.751832160E-02,6.282266110E+03,5.156254270E+02,1.449948340E+04,1.274293990E-03 +Increment 10: Step Time = 1.000,PART-1-1,34,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,35,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,36,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,37,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,38,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,39,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,40,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,41,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,42,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,43,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,44,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,45,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,46,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,47,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,48,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,49,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 diff --git a/reference/shellNL/shellNL stresses.csv b/reference/shellNL/shellNL stresses.csv new file mode 100644 index 0000000..89093bd --- /dev/null +++ b/reference/shellNL/shellNL stresses.csv @@ -0,0 +1,289 @@ +Frame,Part Instance Name, Element Label, Node Label,Section Point, S-S11, S-S22, S-S33, S-S12 +Increment 10: Step Time = 1.000,PART-1-1,1,1,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",5.842519530E+04,1.947512500E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,1,1,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-5.842390620E+04,-1.947457810E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,1,10,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.129284770E+04,1.164291560E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,1,10,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.129343950E+04,-1.164235700E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,1,17,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-4.746073830E+04,-1.582024380E+05,0.000000000E+00,-1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,1,17,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",4.746164060E+04,1.582054690E+05,0.000000000E+00,1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,1,34,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,1,34,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,2,10,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.129284770E+04,1.164291560E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,2,10,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.129343950E+04,-1.164235700E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,2,11,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.922590620E+05,1.462908440E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,2,11,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.922560470E+05,-1.462848280E+05,0.000000000E+00,-9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,2,34,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,2,34,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,2,35,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,2,35,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,-7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,3,2,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",3.423297500E+05,3.423297500E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,3,2,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-3.423234380E+05,-3.423234380E+05,0.000000000E+00,-2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,3,11,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.922560470E+05,-1.462848280E+05,0.000000000E+00,-9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,3,11,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.922590620E+05,1.462908440E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,3,12,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.462908440E+05,1.922590620E+05,0.000000000E+00,9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,3,12,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.462848440E+05,-1.922560470E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,3,35,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,3,35,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,-7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,4,16,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.786850590E+04,5.956166410E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,4,16,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.786817190E+04,-5.956060940E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,4,17,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-4.746073830E+04,-1.582024380E+05,0.000000000E+00,-1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,4,17,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",4.746164060E+04,1.582054690E+05,0.000000000E+00,1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,4,34,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,4,34,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,4,36,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,4,36,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,-5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,5,34,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,5,34,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,5,35,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,5,35,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,-7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,5,36,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,-5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,5,36,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,5,37,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422360E+03,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,5,37,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324136720E+03,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,6,12,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.462908440E+05,1.922590620E+05,0.000000000E+00,9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,6,12,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.462848440E+05,-1.922560470E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,6,13,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.164235700E+05,1.129344040E+04,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,6,13,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.164291560E+05,-1.129284860E+04,0.000000000E+00,-2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,6,35,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,6,35,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,-7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,6,37,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422360E+03,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,6,37,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324136720E+03,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,7,4,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.421875000E-02,7.324218750E-02,0.000000000E+00,1.953125000E-03 +Increment 10: Step Time = 1.000,PART-1-1,7,4,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",7.226562500E-02,7.421875000E-02,0.000000000E+00,-1.953125000E-03 +Increment 10: Step Time = 1.000,PART-1-1,7,15,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-5.956060940E+04,-1.786817190E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,7,15,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",5.956166410E+04,1.786850590E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,7,16,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.786850590E+04,5.956166410E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,7,16,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.786817190E+04,-5.956060940E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,7,36,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,7,36,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,-5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,8,14,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.582024380E+05,-4.746074220E+04,0.000000000E+00,-1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,8,14,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.582054840E+05,4.746164060E+04,0.000000000E+00,1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,8,15,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-5.956060940E+04,-1.786817190E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,8,15,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",5.956166410E+04,1.786850590E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,8,36,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,8,36,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,-5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,8,37,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324136720E+03,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,8,37,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422360E+03,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,9,3,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.947457500E+05,-5.842390620E+04,0.000000000E+00,4.882812500E-04 +Increment 10: Step Time = 1.000,PART-1-1,9,3,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.947512500E+05,5.842519530E+04,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,9,13,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.164235700E+05,1.129344040E+04,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,9,13,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.164291560E+05,-1.129284860E+04,0.000000000E+00,-2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,9,14,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.582024380E+05,-4.746074220E+04,0.000000000E+00,-1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,9,14,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.582054840E+05,4.746164060E+04,0.000000000E+00,1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,9,37,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324136720E+03,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,9,37,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422360E+03,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,10,5,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-5.842390620E+04,-1.947457810E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,10,5,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",5.842519530E+04,1.947512500E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,10,18,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.129284770E+04,1.164291560E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,10,18,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.129343950E+04,-1.164235700E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,10,25,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-4.746073830E+04,-1.582024380E+05,0.000000000E+00,-1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,10,25,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",4.746164060E+04,1.582054690E+05,0.000000000E+00,1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,10,38,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,10,38,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,11,18,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.129284770E+04,1.164291560E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,11,18,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.129343950E+04,-1.164235700E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,11,19,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.922590620E+05,1.462908440E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,11,19,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.922560470E+05,-1.462848280E+05,0.000000000E+00,-9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,11,38,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,11,38,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,11,39,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,11,39,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,-7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,12,2,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",3.423297500E+05,3.423297500E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,12,2,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-3.423234380E+05,-3.423234380E+05,0.000000000E+00,-2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,12,19,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.922560470E+05,-1.462848280E+05,0.000000000E+00,-9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,12,19,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.922590620E+05,1.462908440E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,12,20,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.462908440E+05,1.922590620E+05,0.000000000E+00,9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,12,20,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.462848440E+05,-1.922560470E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,12,39,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,12,39,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,-7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,13,24,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.786850590E+04,5.956166410E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,13,24,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.786817190E+04,-5.956060940E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,13,25,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-4.746073830E+04,-1.582024380E+05,0.000000000E+00,-1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,13,25,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",4.746164060E+04,1.582054690E+05,0.000000000E+00,1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,13,38,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,13,38,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,13,40,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,13,40,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,-5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,14,38,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,14,38,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,14,39,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,14,39,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,-7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,14,40,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,-5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,14,40,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,14,41,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422360E+03,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,14,41,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324136720E+03,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,15,20,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.462908440E+05,1.922590620E+05,0.000000000E+00,9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,15,20,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.462848440E+05,-1.922560470E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,15,21,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.164235700E+05,1.129344040E+04,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,15,21,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.164291560E+05,-1.129284860E+04,0.000000000E+00,-2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,15,39,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,15,39,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,-7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,15,41,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422360E+03,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,15,41,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324136720E+03,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,16,7,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.421875000E-02,7.324218750E-02,0.000000000E+00,1.953125000E-03 +Increment 10: Step Time = 1.000,PART-1-1,16,7,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",7.226562500E-02,7.421875000E-02,0.000000000E+00,-1.953125000E-03 +Increment 10: Step Time = 1.000,PART-1-1,16,23,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-5.956060940E+04,-1.786817190E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,16,23,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",5.956166410E+04,1.786850590E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,16,24,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.786850590E+04,5.956166410E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,16,24,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.786817190E+04,-5.956060940E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,16,40,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,16,40,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,-5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,17,22,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.582024380E+05,-4.746074220E+04,0.000000000E+00,-1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,17,22,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.582054840E+05,4.746164060E+04,0.000000000E+00,1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,17,23,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-5.956060940E+04,-1.786817190E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,17,23,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",5.956166410E+04,1.786850590E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,17,40,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,17,40,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,-5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,17,41,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324136720E+03,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,17,41,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422360E+03,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,18,6,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.947457500E+05,-5.842390620E+04,0.000000000E+00,4.882812500E-04 +Increment 10: Step Time = 1.000,PART-1-1,18,6,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.947512500E+05,5.842519530E+04,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,18,21,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.164235700E+05,1.129344040E+04,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,18,21,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.164291560E+05,-1.129284860E+04,0.000000000E+00,-2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,18,22,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.582024380E+05,-4.746074220E+04,0.000000000E+00,-1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,18,22,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.582054840E+05,4.746164060E+04,0.000000000E+00,1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,18,41,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324136720E+03,0.000000000E+00,-5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,18,41,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422360E+03,0.000000000E+00,5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,19,2,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",3.423297500E+05,3.423297500E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,19,2,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-3.423234380E+05,-3.423234380E+05,0.000000000E+00,-2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,19,12,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.462848440E+05,-1.922560470E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,19,12,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.462908440E+05,1.922590620E+05,0.000000000E+00,9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,19,19,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.922560470E+05,-1.462848280E+05,0.000000000E+00,-9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,19,19,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.922590620E+05,1.462908440E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,19,42,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,-7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,19,42,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,20,18,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.129284770E+04,1.164291560E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,20,18,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.129343950E+04,-1.164235700E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,20,19,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.922590620E+05,1.462908440E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,20,19,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.922560470E+05,-1.462848280E+05,0.000000000E+00,-9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,20,42,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,-7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,20,42,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,20,43,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,20,43,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,21,5,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-5.842390620E+04,-1.947457810E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,21,5,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",5.842519530E+04,1.947512500E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,21,18,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.129284770E+04,1.164291560E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,21,18,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.129343950E+04,-1.164235700E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,21,26,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-4.746074220E+04,-1.582024380E+05,0.000000000E+00,1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,21,26,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",4.746164060E+04,1.582054840E+05,0.000000000E+00,-1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,21,43,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,21,43,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,22,12,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.462848440E+05,-1.922560470E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,22,12,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.462908440E+05,1.922590620E+05,0.000000000E+00,9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,22,13,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.164291560E+05,-1.129284860E+04,0.000000000E+00,-2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,22,13,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.164235700E+05,1.129344040E+04,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,22,42,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,-7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,22,42,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,22,44,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422850E+03,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,22,44,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324135740E+03,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,23,42,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,-7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,23,42,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,23,43,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,23,43,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,23,44,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324135740E+03,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,23,44,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422850E+03,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,23,45,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,-5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,23,45,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,24,26,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-4.746074220E+04,-1.582024380E+05,0.000000000E+00,1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,24,26,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",4.746164060E+04,1.582054840E+05,0.000000000E+00,-1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,24,27,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.786817190E+04,-5.956060940E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,24,27,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.786850590E+04,5.956166410E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,24,43,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,24,43,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,24,45,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,-5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,24,45,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,25,3,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.947512500E+05,5.842519530E+04,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,25,3,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.947457500E+05,-5.842390620E+04,0.000000000E+00,4.882812500E-04 +Increment 10: Step Time = 1.000,PART-1-1,25,13,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.164291560E+05,-1.129284860E+04,0.000000000E+00,-2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,25,13,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.164235700E+05,1.129344040E+04,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,25,29,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.582054840E+05,4.746164060E+04,0.000000000E+00,-1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,25,29,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.582024380E+05,-4.746074220E+04,0.000000000E+00,1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,25,44,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422850E+03,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,25,44,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324135740E+03,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,26,28,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-5.956060940E+04,-1.786817190E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,26,28,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",5.956166410E+04,1.786850780E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,26,29,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.582024380E+05,-4.746074220E+04,0.000000000E+00,1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,26,29,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.582054840E+05,4.746164060E+04,0.000000000E+00,-1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,26,44,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422850E+03,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,26,44,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324135740E+03,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,26,45,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,26,45,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,-5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,27,8,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",7.421875000E-02,7.617187500E-02,0.000000000E+00,1.953125000E-03 +Increment 10: Step Time = 1.000,PART-1-1,27,8,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.421875000E-02,7.421875000E-02,0.000000000E+00,-1.953125000E-03 +Increment 10: Step Time = 1.000,PART-1-1,27,27,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.786817190E+04,-5.956060940E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,27,27,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.786850590E+04,5.956166410E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,27,28,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-5.956060940E+04,-1.786817190E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,27,28,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",5.956166410E+04,1.786850780E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,27,45,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,27,45,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,-5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,28,2,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",3.423297500E+05,3.423297500E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,28,2,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-3.423234380E+05,-3.423234380E+05,0.000000000E+00,-2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,28,11,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.922560470E+05,-1.462848280E+05,0.000000000E+00,-9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,28,11,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.922590620E+05,1.462908440E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,28,20,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.462908440E+05,1.922590620E+05,0.000000000E+00,9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,28,20,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.462848440E+05,-1.922560470E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,28,46,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,-7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,28,46,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,29,10,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.129284770E+04,1.164291560E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,29,10,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.129343950E+04,-1.164235700E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,29,11,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.922590620E+05,1.462908440E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,29,11,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.922560470E+05,-1.462848280E+05,0.000000000E+00,-9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,29,46,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,-7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,29,46,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,29,47,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,29,47,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,30,1,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-5.842390620E+04,-1.947457810E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,30,1,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",5.842519530E+04,1.947512500E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,30,10,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.129284770E+04,1.164291560E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,30,10,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.129343950E+04,-1.164235700E+05,0.000000000E+00,2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,30,30,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-4.746074220E+04,-1.582024380E+05,0.000000000E+00,1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,30,30,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",4.746164060E+04,1.582054840E+05,0.000000000E+00,-1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,30,47,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,30,47,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,31,20,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.462848440E+05,-1.922560470E+05,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,31,20,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.462908440E+05,1.922590620E+05,0.000000000E+00,9.765625000E-04 +Increment 10: Step Time = 1.000,PART-1-1,31,21,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.164291560E+05,-1.129284860E+04,0.000000000E+00,-2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,31,21,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.164235700E+05,1.129344040E+04,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,31,46,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,-7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,31,46,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,31,48,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422850E+03,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,31,48,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324135740E+03,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,32,46,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-1.028310310E+05,-1.028310310E+05,0.000000000E+00,-7.438760940E+04 +Increment 10: Step Time = 1.000,PART-1-1,32,46,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",1.028341250E+05,1.028341250E+05,0.000000000E+00,7.438745310E+04 +Increment 10: Step Time = 1.000,PART-1-1,32,47,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,32,47,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,32,48,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324135740E+03,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,32,48,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422850E+03,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,32,49,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,-5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,32,49,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,33,30,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-4.746074220E+04,-1.582024380E+05,0.000000000E+00,1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,33,30,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",4.746164060E+04,1.582054840E+05,0.000000000E+00,-1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,33,31,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.786817190E+04,-5.956060940E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,33,31,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.786850590E+04,5.956166410E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,33,47,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",-5.323422850E+03,7.259001560E+04,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,33,47,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",5.324135740E+03,-7.258690620E+04,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,33,49,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,-5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,33,49,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,34,6,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.947512500E+05,5.842519530E+04,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,34,6,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.947457500E+05,-5.842390620E+04,0.000000000E+00,4.882812500E-04 +Increment 10: Step Time = 1.000,PART-1-1,34,21,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.164291560E+05,-1.129284860E+04,0.000000000E+00,-2.441406250E-04 +Increment 10: Step Time = 1.000,PART-1-1,34,21,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.164235700E+05,1.129344040E+04,0.000000000E+00,0.000000000E+00 +Increment 10: Step Time = 1.000,PART-1-1,34,33,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.582054840E+05,4.746164060E+04,0.000000000E+00,-1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,34,33,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.582024380E+05,-4.746074220E+04,0.000000000E+00,1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,34,48,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422850E+03,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,34,48,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324135740E+03,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,35,32,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-5.956060940E+04,-1.786817190E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,35,32,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",5.956166410E+04,1.786850780E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,35,33,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.582024380E+05,-4.746074220E+04,0.000000000E+00,1.777732030E+04 +Increment 10: Step Time = 1.000,PART-1-1,35,33,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.582054840E+05,4.746164060E+04,0.000000000E+00,-1.777733200E+04 +Increment 10: Step Time = 1.000,PART-1-1,35,48,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.259001560E+04,-5.323422850E+03,0.000000000E+00,-5.219074610E+04 +Increment 10: Step Time = 1.000,PART-1-1,35,48,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-7.258690620E+04,5.324135740E+03,0.000000000E+00,5.219067970E+04 +Increment 10: Step Time = 1.000,PART-1-1,35,49,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,35,49,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,-5.537141410E+04 +Increment 10: Step Time = 1.000,PART-1-1,36,9,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",7.421875000E-02,7.617187500E-02,0.000000000E+00,1.953125000E-03 +Increment 10: Step Time = 1.000,PART-1-1,36,9,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",7.421875000E-02,7.421875000E-02,0.000000000E+00,-1.953125000E-03 +Increment 10: Step Time = 1.000,PART-1-1,36,31,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-1.786817190E+04,-5.956060940E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,36,31,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",1.786850590E+04,5.956166410E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,36,32,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-5.956060940E+04,-1.786817190E+04,0.000000000E+00,2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,36,32,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",5.956166410E+04,1.786850780E+04,0.000000000E+00,-2.084639450E+04 +Increment 10: Step Time = 1.000,PART-1-1,36,49,"shell < MATERIAL-1 > < 5 section points > : SNEG, (fraction = -1.0)",-3.301455860E+04,-3.301455860E+04,0.000000000E+00,5.537136720E+04 +Increment 10: Step Time = 1.000,PART-1-1,36,49,"shell < MATERIAL-1 > < 5 section points > : SPOS, (fraction = 1.0)",3.301550780E+04,3.301550780E+04,0.000000000E+00,-5.537141410E+04 diff --git a/reference/shellR/shellR.inp b/reference/shellNL/shellNL.inp similarity index 97% rename from reference/shellR/shellR.inp rename to reference/shellNL/shellNL.inp index 1cd748d..849d3a1 100644 --- a/reference/shellR/shellR.inp +++ b/reference/shellNL/shellNL.inp @@ -1,5 +1,5 @@ *Heading -** Job name: shellR Model name: Model-1 +** Job name: shellNL Model name: Model-1-NL ** Generated by: Abaqus/CAE Learning Edition 2024 *Preprint, echo=NO, model=NO, history=NO, contact=NO ** @@ -56,7 +56,7 @@ 47, 1.66666663, -3.33333325, 0. 48, 3.33333325, -1.66666663, 0. 49, 3.33333325, -3.33333325, 0. -*Element, type=S4R +*Element, type=S4 1, 1, 10, 34, 17 2, 10, 11, 35, 34 3, 11, 2, 12, 35 @@ -140,9 +140,9 @@ Set-2, 6, 6 ** ** STEP: Step-1 ** -*Step, name=Step-1, nlgeom=NO +*Step, name=Step-1, nlgeom=YES *Static -1., 1., 1e-05, 1. +0.1, 1., 0.001, 0.1 ** ** LOADS ** diff --git a/reference/shellR/shellR displacements.csv b/reference/shellR/shellR displacements.csv deleted file mode 100644 index f1d06ff..0000000 --- a/reference/shellR/shellR displacements.csv +++ /dev/null @@ -1,50 +0,0 @@ -Part Instance Name, Node Label, U-U1, U-U2, U-U3, UR-UR1, UR-UR2, UR-UR3 -PART-1-1,1,0.000000000E+00,0.000000000E+00,-1.331558420E-32,-1.970332920E-32,0.000000000E+00,0.000000000E+00 -PART-1-1,2,-5.841562080E-39,-4.221586230E-38,-2.455982390E-05,1.182512440E-20,-2.259823100E-21,-3.091293840E-39 -PART-1-1,3,0.000000000E+00,0.000000000E+00,-1.331558420E-32,0.000000000E+00,1.970332920E-32,0.000000000E+00 -PART-1-1,4,0.000000000E+00,0.000000000E+00,-8.347285490E-34,-2.440103850E-33,2.440103850E-33,0.000000000E+00 -PART-1-1,5,0.000000000E+00,0.000000000E+00,-1.331558420E-32,1.970332920E-32,0.000000000E+00,0.000000000E+00 -PART-1-1,6,0.000000000E+00,0.000000000E+00,-1.331558420E-32,0.000000000E+00,-1.970332920E-32,0.000000000E+00 -PART-1-1,7,0.000000000E+00,0.000000000E+00,-8.347285490E-34,2.440103850E-33,-2.440103850E-33,0.000000000E+00 -PART-1-1,8,0.000000000E+00,0.000000000E+00,-8.347285490E-34,2.440103850E-33,2.440103850E-33,0.000000000E+00 -PART-1-1,9,0.000000000E+00,0.000000000E+00,-8.347285490E-34,-2.440103850E-33,-2.440103850E-33,0.000000000E+00 -PART-1-1,10,-9.340510460E-39,2.282739110E-23,-5.128820250E-06,-5.520078050E-06,-2.659617300E-21,-1.126454790E-39 -PART-1-1,11,7.453514940E-39,3.347210340E-23,-1.652319220E-05,-8.192502720E-06,2.111991020E-21,-1.428400980E-39 -PART-1-1,12,3.347210340E-23,-4.735159870E-39,-1.652319220E-05,6.633812820E-22,8.192502720E-06,1.333020200E-39 -PART-1-1,13,2.282739110E-23,-1.713440220E-38,-5.128820250E-06,4.277562190E-21,5.520078050E-06,2.811129430E-39 -PART-1-1,14,0.000000000E+00,0.000000000E+00,-4.980328960E-33,9.272010730E-35,1.376352830E-32,0.000000000E+00 -PART-1-1,15,0.000000000E+00,0.000000000E+00,-4.445146580E-34,-1.384767610E-33,7.223171810E-33,0.000000000E+00 -PART-1-1,16,0.000000000E+00,0.000000000E+00,-4.445146580E-34,-7.223171810E-33,1.384767610E-33,0.000000000E+00 -PART-1-1,17,0.000000000E+00,0.000000000E+00,-4.980328960E-33,-1.376352830E-32,-9.272010730E-35,0.000000000E+00 -PART-1-1,18,-1.099882110E-38,-2.282739110E-23,-5.128820250E-06,5.520078050E-06,-3.218899240E-21,2.564589190E-39 -PART-1-1,19,1.901636000E-38,-3.347210340E-23,-1.652319220E-05,8.192502720E-06,5.455173340E-21,1.173231530E-39 -PART-1-1,20,-3.347210340E-23,-9.621524050E-39,-1.652319220E-05,2.013808970E-21,-8.192502720E-06,3.963135500E-39 -PART-1-1,21,-2.282739110E-23,5.468459360E-39,-5.128820250E-06,-1.144154870E-21,-5.520078050E-06,2.990265830E-39 -PART-1-1,22,0.000000000E+00,0.000000000E+00,-4.980328960E-33,-9.272010730E-35,-1.376352830E-32,0.000000000E+00 -PART-1-1,23,0.000000000E+00,0.000000000E+00,-4.445146580E-34,1.384767610E-33,-7.223171810E-33,0.000000000E+00 -PART-1-1,24,0.000000000E+00,0.000000000E+00,-4.445146580E-34,7.223171810E-33,-1.384767610E-33,0.000000000E+00 -PART-1-1,25,0.000000000E+00,0.000000000E+00,-4.980328960E-33,1.376352830E-32,9.272010730E-35,0.000000000E+00 -PART-1-1,26,0.000000000E+00,0.000000000E+00,-4.980328960E-33,1.376352830E-32,-9.272010730E-35,0.000000000E+00 -PART-1-1,27,0.000000000E+00,0.000000000E+00,-4.445146580E-34,7.223171810E-33,1.384767610E-33,0.000000000E+00 -PART-1-1,28,0.000000000E+00,0.000000000E+00,-4.445146580E-34,1.384767610E-33,7.223171810E-33,0.000000000E+00 -PART-1-1,29,0.000000000E+00,0.000000000E+00,-4.980328960E-33,-9.272010730E-35,1.376352830E-32,0.000000000E+00 -PART-1-1,30,0.000000000E+00,0.000000000E+00,-4.980328960E-33,-1.376352830E-32,9.272010730E-35,0.000000000E+00 -PART-1-1,31,0.000000000E+00,0.000000000E+00,-4.445146580E-34,-7.223171810E-33,-1.384767610E-33,0.000000000E+00 -PART-1-1,32,0.000000000E+00,0.000000000E+00,-4.445146580E-34,-1.384767610E-33,-7.223171810E-33,0.000000000E+00 -PART-1-1,33,0.000000000E+00,0.000000000E+00,-4.980328960E-33,9.272010730E-35,-1.376352830E-32,0.000000000E+00 -PART-1-1,34,5.657543960E-24,1.990244950E-23,-4.090960830E-06,-4.837134840E-06,1.424931610E-06,-6.313478650E-25 -PART-1-1,35,1.965293750E-23,1.965293750E-23,-1.253621300E-05,-4.676389840E-06,4.676389840E-06,-2.850357380E-39 -PART-1-1,36,7.383441460E-24,7.383441460E-24,-1.533419780E-06,-1.768650120E-06,1.768650120E-06,-2.343029890E-39 -PART-1-1,37,1.990244950E-23,5.657543960E-24,-4.090960830E-06,-1.424931610E-06,4.837134840E-06,6.313478650E-25 -PART-1-1,38,-5.657543960E-24,-1.990244950E-23,-4.090960830E-06,4.837134840E-06,-1.424931610E-06,-6.313478650E-25 -PART-1-1,39,-1.965293750E-23,-1.965293750E-23,-1.253621300E-05,4.676389840E-06,-4.676389840E-06,-6.227405410E-39 -PART-1-1,40,-7.383441460E-24,-7.383441460E-24,-1.533419780E-06,1.768650120E-06,-1.768650120E-06,-3.769452230E-39 -PART-1-1,41,-1.990244950E-23,-5.657543960E-24,-4.090960830E-06,1.424931610E-06,-4.837134840E-06,6.313478650E-25 -PART-1-1,42,1.965293750E-23,-1.965293750E-23,-1.253621300E-05,4.676389840E-06,4.676389840E-06,4.802227420E-39 -PART-1-1,43,5.657543960E-24,-1.990244950E-23,-4.090960830E-06,4.837134840E-06,1.424931610E-06,6.313478650E-25 -PART-1-1,44,1.990244950E-23,-5.657543960E-24,-4.090960830E-06,1.424931610E-06,4.837134840E-06,-6.313478650E-25 -PART-1-1,45,7.383441460E-24,-7.383441460E-24,-1.533419780E-06,1.768650120E-06,1.768650120E-06,2.502447210E-39 -PART-1-1,46,-1.965293750E-23,1.965293750E-23,-1.253621300E-05,-4.676389840E-06,-4.676389840E-06,7.125896960E-40 -PART-1-1,47,-5.657543960E-24,1.990244950E-23,-4.090960830E-06,-4.837134840E-06,-1.424931610E-06,6.313478650E-25 -PART-1-1,48,-1.990244950E-23,5.657543960E-24,-4.090960830E-06,-1.424931610E-06,-4.837134840E-06,-6.313478650E-25 -PART-1-1,49,-7.383441460E-24,7.383441460E-24,-1.533419780E-06,-1.768650120E-06,-1.768650120E-06,-2.681194030E-39 diff --git a/reference/shellR/shellR reactions.csv b/reference/shellR/shellR reactions.csv deleted file mode 100644 index 3417c77..0000000 --- a/reference/shellR/shellR reactions.csv +++ /dev/null @@ -1,50 +0,0 @@ -Part Instance Name, Node Label, RF-RF1, RF-RF2, RF-RF3, RM-RM1, RM-RM2, RM-RM3 -PART-1-1,1,1.133987550E-29,-2.402367760E-15,1.331558400E+04,1.970333010E+04,-1.364242050E-11,-1.240831900E-29 -PART-1-1,2,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,3,2.934507450E-12,-2.842170940E-13,1.331558400E+04,1.978150980E-11,-1.970333010E+04,2.276204690E-29 -PART-1-1,4,1.911357090E-13,1.911357090E-13,8.347285770E+02,2.440104000E+03,-2.440104000E+03,0.000000000E+00 -PART-1-1,5,9.473904270E-14,-1.608161090E-12,1.331558400E+04,-1.970333010E+04,-9.777068040E-12,1.461128720E-29 -PART-1-1,6,2.402367760E-15,-1.045240700E-29,1.331558400E+04,-3.183231460E-12,1.970333010E+04,7.264527250E-30 -PART-1-1,7,-1.657630980E-15,3.772985070E-13,8.347285770E+02,-2.440104000E+03,2.440104000E+03,0.000000000E+00 -PART-1-1,8,1.911357090E-13,-1.911357090E-13,8.347285770E+02,-2.440104000E+03,-2.440104000E+03,0.000000000E+00 -PART-1-1,9,-1.911357090E-13,1.911357090E-13,8.347285770E+02,2.440104000E+03,2.440104000E+03,0.000000000E+00 -PART-1-1,10,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,11,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,12,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,13,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,14,1.324633000E-12,3.782636370E-13,4.980329100E+03,-9.272010800E+01,-1.376352830E+04,-7.515714870E-15 -PART-1-1,15,3.802131140E-13,-1.916272050E-13,4.445146790E+02,1.384767580E+03,-7.223171880E+03,-9.808467890E-15 -PART-1-1,16,-2.149133070E-15,3.802131140E-13,4.445146790E+02,7.223171880E+03,-1.384767580E+03,9.808467890E-15 -PART-1-1,17,1.887855650E-13,-1.911915040E-13,4.980329100E+03,1.376352830E+04,9.272010800E+01,7.515714870E-15 -PART-1-1,18,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,19,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,20,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,21,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,22,-5.667207150E-13,-1.887855650E-13,4.980329100E+03,9.272010800E+01,1.376352830E+04,-7.515714870E-15 -PART-1-1,23,5.671771650E-13,-5.662850830E-13,4.445146790E+02,-1.384767580E+03,7.223171880E+03,-9.808467890E-15 -PART-1-1,24,2.149118250E-15,3.776991740E-13,4.445146790E+02,-7.223171880E+03,1.384767580E+03,9.808467890E-15 -PART-1-1,25,6.924991450E-16,-1.514110990E-12,4.980329100E+03,-1.376352830E+04,-9.272010800E+01,7.515714870E-15 -PART-1-1,26,-2.849096010E-13,8.543647020E-13,4.980329100E+03,-1.376352830E+04,9.272010800E+01,-7.515714870E-15 -PART-1-1,27,-1.916271910E-13,5.671771650E-13,4.445146790E+02,-7.223171880E+03,-1.384767580E+03,-9.808467890E-15 -PART-1-1,28,-5.671771650E-13,2.149118250E-15,4.445146790E+02,-1.384767580E+03,-7.223171880E+03,9.808467890E-15 -PART-1-1,29,8.509378640E-13,2.849096010E-13,4.980329100E+03,9.272010800E+01,-1.376352830E+04,7.515714870E-15 -PART-1-1,30,-1.887855650E-13,-1.911915040E-13,4.980329100E+03,1.376352830E+04,-9.272010800E+01,-7.515714870E-15 -PART-1-1,31,2.149133070E-15,3.802131140E-13,4.445146790E+02,7.223171880E+03,1.384767580E+03,-9.808467890E-15 -PART-1-1,32,1.882210890E-13,-5.705832940E-13,4.445146790E+02,1.384767580E+03,7.223171880E+03,9.808467890E-15 -PART-1-1,33,1.138581740E-12,-3.796486240E-13,4.980329100E+03,-9.272010800E+01,1.376352830E+04,7.515714870E-15 -PART-1-1,34,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,35,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,36,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,37,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,38,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,39,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,40,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,41,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,42,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,43,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,44,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,45,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,46,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,47,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,48,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 -PART-1-1,49,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00,0.000000000E+00 diff --git a/reference/shellR/shellR stresses.csv b/reference/shellR/shellR stresses.csv deleted file mode 100644 index aebfbfb..0000000 --- a/reference/shellR/shellR stresses.csv +++ /dev/null @@ -1,289 +0,0 @@ -Part Instance Name, Element Label, Node Label, S-S11, S-S22, S-S33, S-S12 -PART-1-1,1,1,2.911555470E+04,1.718607660E+05,0.000000000E+00,0.000000000E+00 -PART-1-1,1,1,-2.911555470E+04,-1.718607660E+05,0.000000000E+00,0.000000000E+00 -PART-1-1,1,10,-3.172141020E+04,9.182610160E+04,0.000000000E+00,0.000000000E+00 -PART-1-1,1,10,3.172141020E+04,-9.182610160E+04,0.000000000E+00,0.000000000E+00 -PART-1-1,1,17,-2.873292190E+04,-1.422034840E+05,0.000000000E+00,-2.535126560E+04 -PART-1-1,1,17,2.873292190E+04,1.422034840E+05,0.000000000E+00,2.535126560E+04 -PART-1-1,1,34,-1.161074020E+04,7.121199220E+04,0.000000000E+00,4.310100000E+04 -PART-1-1,1,34,1.161074020E+04,-7.121199220E+04,0.000000000E+00,-4.310100000E+04 -PART-1-1,2,10,-3.172141020E+04,9.182610160E+04,0.000000000E+00,0.000000000E+00 -PART-1-1,2,10,3.172141020E+04,-9.182610160E+04,0.000000000E+00,0.000000000E+00 -PART-1-1,2,11,1.910542340E+05,1.388793280E+05,0.000000000E+00,0.000000000E+00 -PART-1-1,2,11,-1.910542340E+05,-1.388793280E+05,0.000000000E+00,0.000000000E+00 -PART-1-1,2,34,1.161074020E+04,-7.121199220E+04,0.000000000E+00,-4.310100000E+04 -PART-1-1,2,34,-1.161074020E+04,7.121199220E+04,0.000000000E+00,4.310100000E+04 -PART-1-1,2,35,-9.541686720E+04,-9.541686720E+04,0.000000000E+00,5.235836330E+04 -PART-1-1,2,35,9.541686720E+04,9.541686720E+04,0.000000000E+00,-5.235836330E+04 -PART-1-1,3,2,2.895500940E+05,2.895500940E+05,0.000000000E+00,0.000000000E+00 -PART-1-1,3,2,-2.895500940E+05,-2.895500940E+05,0.000000000E+00,0.000000000E+00 -PART-1-1,3,11,-1.910542340E+05,-1.388793280E+05,0.000000000E+00,0.000000000E+00 -PART-1-1,3,11,1.910542340E+05,1.388793280E+05,0.000000000E+00,0.000000000E+00 -PART-1-1,3,12,1.388793280E+05,1.910542340E+05,0.000000000E+00,0.000000000E+00 -PART-1-1,3,12,-1.388793280E+05,-1.910542340E+05,0.000000000E+00,0.000000000E+00 -PART-1-1,3,35,-9.541686720E+04,-9.541686720E+04,0.000000000E+00,5.235836330E+04 -PART-1-1,3,35,9.541686720E+04,9.541686720E+04,0.000000000E+00,-5.235836330E+04 -PART-1-1,4,16,3.407245700E+04,7.617040620E+04,0.000000000E+00,2.968077340E+04 -PART-1-1,4,16,-3.407245700E+04,-7.617040620E+04,0.000000000E+00,-2.968077340E+04 -PART-1-1,4,17,-2.873292190E+04,-1.422034840E+05,0.000000000E+00,-2.535126560E+04 -PART-1-1,4,17,2.873292190E+04,1.422034840E+05,0.000000000E+00,2.535126560E+04 -PART-1-1,4,34,-1.161074020E+04,7.121199220E+04,0.000000000E+00,4.310100000E+04 -PART-1-1,4,34,1.161074020E+04,-7.121199220E+04,0.000000000E+00,-4.310100000E+04 -PART-1-1,4,36,4.233517190E+04,4.233517190E+04,0.000000000E+00,4.346593750E+04 -PART-1-1,4,36,-4.233517190E+04,-4.233517190E+04,0.000000000E+00,-4.346593750E+04 -PART-1-1,5,34,1.161074020E+04,-7.121199220E+04,0.000000000E+00,-4.310100000E+04 -PART-1-1,5,34,-1.161074020E+04,7.121199220E+04,0.000000000E+00,4.310100000E+04 -PART-1-1,5,35,-9.541686720E+04,-9.541686720E+04,0.000000000E+00,5.235836330E+04 -PART-1-1,5,35,9.541686720E+04,9.541686720E+04,0.000000000E+00,-5.235836330E+04 -PART-1-1,5,36,-4.233517190E+04,-4.233517190E+04,0.000000000E+00,-4.346593750E+04 -PART-1-1,5,36,4.233517190E+04,4.233517190E+04,0.000000000E+00,4.346593750E+04 -PART-1-1,5,37,7.121199220E+04,-1.161074020E+04,0.000000000E+00,4.310100000E+04 -PART-1-1,5,37,-7.121199220E+04,1.161074020E+04,0.000000000E+00,-4.310100000E+04 -PART-1-1,6,12,1.388793280E+05,1.910542340E+05,0.000000000E+00,0.000000000E+00 -PART-1-1,6,12,-1.388793280E+05,-1.910542340E+05,0.000000000E+00,0.000000000E+00 -PART-1-1,6,13,-9.182610160E+04,3.172141020E+04,0.000000000E+00,0.000000000E+00 -PART-1-1,6,13,9.182610160E+04,-3.172141020E+04,0.000000000E+00,0.000000000E+00 -PART-1-1,6,35,-9.541686720E+04,-9.541686720E+04,0.000000000E+00,5.235836330E+04 -PART-1-1,6,35,9.541686720E+04,9.541686720E+04,0.000000000E+00,-5.235836330E+04 -PART-1-1,6,37,7.121199220E+04,-1.161074020E+04,0.000000000E+00,4.310100000E+04 -PART-1-1,6,37,-7.121199220E+04,1.161074020E+04,0.000000000E+00,-4.310100000E+04 -PART-1-1,7,4,3.979462500E+04,3.979462500E+04,0.000000000E+00,2.142787500E+04 -PART-1-1,7,4,-3.979462500E+04,-3.979462500E+04,0.000000000E+00,-2.142787500E+04 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