Files
MultiPhysicsVault/wiki/concepts/Finite Element Thermal Stress Analysis.md
김경종 553842ac3b
Tests / Hermetic test suite (push) Has been cancelled
Tests / Skill frontmatter validation (push) Has been cancelled
modify wiki
2026-06-02 16:57:41 +09:00

6.2 KiB

type, title, complexity, domain, created, updated, address, aliases, tags, status, related, sources, source_refs
type title complexity domain created updated address aliases tags status related sources source_refs
concept Finite Element Thermal Stress Analysis intermediate computational-mechanics 2026-05-29 2026-06-02 c-000070
thermal stress finite element analysis
thermal strain load vector
temperature-induced stress
concept
finite-element-method
thermal-stress
coupled-field
current
Finite Element Heat Transfer and Field Problems
Finite Element Load Vector Assembly
Plane Stress and Plane Strain Elements
Axisymmetric Finite Elements
Displacement-Based Finite Element Formulation
Abaqus Thermal Expansion and Damping Materials
Midas Civil Heat of Hydration and Thermal Stress Analysis
Midas FEA Heat Transfer and Hydration Analysis
Midas NFX Heat Transfer Joule Heating and Thermal Stress
A-First-Course-in-the-Finite-Element-Method
Abaqus-Analysis-User-s-Guide-Volume-III
Midas-Civil-Analysis-Reference
Midas-NFX-Analysis-Manual
source raw_path raw_files md_indices match confidence
A-First-Course-in-the-Finite-Element-Method .raw/AFirstCourseInTheFiniteElementMethod/
AFirstCourseInTheFiniteElementMethod_064.md
AFirstCourseInTheFiniteElementMethod_001.md
AFirstCourseInTheFiniteElementMethod_033.md
AFirstCourseInTheFiniteElementMethod_083.md
64
1
33
83
heuristic-heading-keyword high
source raw_path raw_files md_indices match confidence
Abaqus-Analysis-User-s-Guide-Volume-III .raw/AbaqusAnalysisUserGuide3/
AbaqusAnalysisUserGuide3_062.md
AbaqusAnalysisUserGuide3_061.md
AbaqusAnalysisUserGuide3_005.md
AbaqusAnalysisUserGuide3_002.md
62
61
5
2
heuristic-heading-keyword high
source raw_path raw_files md_indices match confidence
Midas-Civil-Analysis-Reference .raw/MidasCivilAnalysisReference/
MidasCivilAnalysisReference_048.md
MidasCivilAnalysisReference_049.md
48
49
heuristic-heading-keyword high
source raw_path raw_files md_indices match confidence
Midas-NFX-Analysis-Manual .raw/MidasNFXAnalysisManual/
MidasNFXAnalysisManual_010.md
MidasNFXAnalysisManual_012.md
MidasNFXAnalysisManual_007.md
MidasNFXAnalysisManual_011.md
10
12
7
11
heuristic-heading-keyword high

Finite Element Thermal Stress Analysis

Definition

Finite element thermal stress analysis computes stresses caused by temperature-induced strains, especially when expansion or contraction is constrained.

How It Works

The source treats thermal strain as an initial strain contribution. For a uniform temperature change in an isotropic material, thermal strain is proportional to the coefficient of thermal expansion and the temperature change. The constitutive relation is written in terms of mechanical strain minus thermal strain, so the thermal contribution enters the finite element equations as an equivalent nodal force vector.

The same idea is applied to one-dimensional bars, plane stress and plane strain elements, and axisymmetric triangular elements. If the structure is free to expand, thermal strain may produce displacement without stress. If constraints or material incompatibility prevent free expansion, thermal stresses appear.

Abaqus-Analysis-User-s-Guide-Volume-III adds production material definitions for this mechanism: thermal expansion coefficients, reference temperatures, temperature/field dependencies, isotropic/orthotropic/anisotropic expansion, and user-defined expansion increments through UEXPAN.

Midas-Civil-Analysis-Reference adds the civil concrete workflow: hydration heat first defines a temperature and equivalent-age history, then structural stress analysis combines thermal strain, shrinkage, creep, and age-dependent concrete strength.

Midas-NFX-Analysis-Manual adds a general-purpose thermal-stress view: structural elements can be reused as thermal elements by changing the DOF to temperature, thermal gradients and fluxes are recovered as element results, and composite laminates can receive average temperature change plus through-thickness gradient terms that generate membrane and bending resultants.

Why It Matters

Thermal loading is not just another external force. It changes the strain state inside the element and can create stress only through constraint, incompatibility, or temperature gradients. Treating it as an equivalent nodal contribution keeps the global equation format compatible with the displacement formulation.

Connections

Sources