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Cook's membrane

StaticIn development

Sensitivity to a skewed mesh under combined bending/shear

Source:
MacNeal-Harder (1985)
Tolerance:
2%

Problem statement

Geometry
Tapered cantilever panel with corners at (0,0), (48,44), (48,60), (0,44); thickness 1 (consistent units).
Material
Plane stress, E = 1, ν = 1/3.
Boundary conditions
Fully clamped along the left edge (x=0); a distributed shear load totaling 1 unit along the right edge (x=48).
Measured quantity
Vertical deflection at the midpoint of the loaded edge (point C, x=48).

Script

Lands with the scripting engine (see Documentation) — this setup will be runnable from commands, no manual rebuild needed.

Results comparison

The solver core is still in development — there's no result yet. It'll appear here right after the first run, no retouching.

Updated: not yet run

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