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type title complexity domain aliases created updated address tags status related sources source_refs
concept Scordelis-Lo Shell Benchmark intermediate computational-mechanics
Scordelis-Lo shell
cylindrical Scordelis-Lo shell
Scordelis Lo roof
2026-05-28 2026-05-28 c-000024
concept
finite-element-method
shell-elements
benchmark
current
On-the-Finite-Element-Analysis-of-Shell-Structures
Shell Structure Asymptotic Behavior
Shell Element Benchmark Testing
Four-Node-Quadrilateral-Shell-Element-MITC4
MITC4 Shell Element
Continuum Mechanics Based Four-Node Shell Element
Static Equilibrium Equation Solvers
On-the-Finite-Element-Analysis-of-Shell-Structures
Four-Node-Quadrilateral-Shell-Element-MITC4
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On-the-Finite-Element-Analysis-of-Shell-Structures .raw/쉘구조물의유한요소해석에대하여/
쉘구조물의유한요소해석에대하여_002.md
쉘구조물의유한요소해석에대하여_001.md
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Four-Node-Quadrilateral-Shell-Element-MITC4 .raw/FourNodeQuadrilateralShellElementMITC4/
FourNodeQuadrilateralShellElementMITC4_001.md
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Scordelis-Lo Shell Benchmark

Definition

The Scordelis-Lo shell benchmark is a classical cylindrical shell problem used to evaluate shell finite elements under bending and membrane action.

How It Is Used

In the MITC4 source, the shell is loaded by dead weight and symmetry allows one quarter of the structure to be modeled. The response quantity is the displacement at point B, and mesh refinement is used to compare MITC4 convergence with an RDKT reference element and an analytical reference.

On-the-Finite-Element-Analysis-of-Shell-Structures uses the Scordelis-Lo roof shell as an asymptotic-behavior example. The paper identifies it as a mixed-dominated shell benchmark with an approximate load scaling factor of rho = 1.75, which makes it useful for exposing locking and non-uniform convergence.

Why It Matters

The benchmark is useful because shell elements must couple membrane and bending behavior without becoming artificially stiff. Poor shell formulations can pass simple tests yet converge slowly or incorrectly on this curved-shell problem.

Reported Trend

The source reports MITC4 displacement magnitudes converging from about 3.43 on a 4x4 quadrilateral mesh to about 3.61 on 32x32 and 64x64 meshes. The RDKT comparison converges to about 3.60 on the same refinement sequence.

Connections

Sources