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NAFEMS Linear Static Benchmarks

Cylindrical Shell Under Edge Moment

Elliptic Membrane Under Pressure

Tapered Geometry - Edge Loading

Axisymmetric Cylinder Sphere under Internal Pressure

Skew Plate under Normal Pressure

Cylindrical Shell under Pressure Load

Z-Section Cantilever Under Torsion Bending

Tapered Geometry - Gravity Loading

Radial Loading of Circular Membrane

Hemisphere Under External Pressure

Hemisphere Under Point Loads

NAFEMS Nonlinear Analysis Benchmarks

NAFEMS Thermal Benchmarks

NAFEMS Natural Frequency Benchmarks

NAFEMS Forced Vibration Benchmarks

NAFEMS Composites Benchmarks

Skew Plate under Normal Pressure

Calculate the maximum principal stress at the center E of a skew plate under a normal pressure of 0.7 KPa.

File Name

Open drive letter:\Users\Public\Public Documents\SOLIDWORKS\SOLIDWORKS version\samples\Simulation Examples\Verification\NAFEMS_IC13.SLDPRT.

Study Type

Static

Mesh Type

Shell mesh

Shell Parameters

Shell thickness = 0.01 m - Thin shell formulation

Material Properties

Modulus of elasticity = 210 X 10³ MPa
Poisson's ratio = 0.3

Results

Component	Reference	SOLIDWORKS Simulation
Maximum principal stress at point E (MPa)	0.802	0.806

Reference

NAFEMS Publication P07, The International Association for the Engineering Analysis Community, "Linear Statics Benchmarks VOL. 1", D. Hitchings, A.Kamoulakos, G.A. Davies, VOL. 1, October, 1987.

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