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Static Analysis
SS-V: 1220 Displacements in Hemispherical Shell
Test No. VS23 Find displacements in a hemispherical shell.

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- Introduction
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- Static Analysis
  - SS-V: 1000 Straight Cantilever Beam
    Test No. VS01 Find tip deflections of a cantilever beam when subjected to extension, shear, and twisting loads.
  - SS-V: 1010 Twisted Cantilever Beam
    Test No. VS02 Find tip deflections of a twisted cantilever beam when subjected to shear loads.
  - SS-V: 1020 Curved Beam
    Test No. VS03 Find tip deflections of a curved beam when subjected to in-plane and out-of-plane loads.
  - SS-V: 1030 Simply Supported Thin Plate
    Test No. VS04 Obtain the displacement at the center of a simple supported thin plate for concentrated load and uniform pressure load.
  - SS-V: 1040 Clamped Thin Plate
    Test No. VS05 Obtain the displacement at the center of a clamped thin plate for concentrated load and uniform pressure load.
  - SS-V: 1050 Tapered Solid Bar
    Test No. VS06 Determine the maximum axial deflection and axial stress at the mid-length for a tapered solid bar.
  - SS-V: 1060 Cantilever Plate
    Test No. VS07 Find bending stress at fixed end for a cantilevered plate subjected to a vertical shear load of 120 lbs.
  - SS-V: 1070 Plate with a Hole
    Test No. VS08 Find the maximum stress of a plate with a hole.
  - SS-V: 1080 Scordelis-Lo Roof
    Test No. VS09 Find the maximum Z displacement for a curved cylindrical dome.
  - SS-V: 1090 Stepped Shaft with Fillet
    Test No. VS10 Find the stress concentration in a filleted notch.
  - SS-V: 1100 Raasch Challenge
    Test No. VS11 Find the tip displacement at the free end of a thick, doubly curved beam.
  - SS-V: 1110 Notched Plate
    Test No. VS12 Find Sx stress in the notch and top face of a notched plate.
  - SS-V: 1120 Simply Supported Beam with Mid-span Load
    Test No. VS13 Find the max displacement and stress for a pinned beam with load at the midpoint.
  - SS-V: 1130 Skew Plate Under Pressure
    Test No. VS14 Find the maximum principle stress at the skew plate center at point E.
  - SS-V: 1140 Stress Concentration of Filleted Bar
    Test No. VS15 Find maximum normal stress for two configurations of a filleted bar.
  - SS-V: 1150 Buckling
    Test No. VS16 Find the critical compression load at which the cantilever beam buckles.
  - SS-V: 1160 Stress Concentration in a Groove Shaft
    Test No. VS17 Find the stress concentration in a grooved shaft.
  - SS-V: 1170 Stress Concentration of a Plate with Eccentric Hole
    Test No. VS18 Find the stress concentration in a plate with eccentric hole.
  - SS-V: 1180 Stress Concentration in a Filleted Notch
    Test No. VS19 Find the stress concentration in a filleted notch when torque is applied.
  - SS-V: 1190 Stress Concentration of a Plate with Semi-circular Holes
    Test No. VS20 Find the stress concentration in a plate with semi-circular holes.
  - SS-V: 1200 Tangential Edge Stress in an Elliptic Membrane
    Test No. VS21 Find the tangential edge stress in an elliptic membrane.
  - SS-V: 1210 Tangential Stress for a Cylindrical Shell
    Test No. VS22 Find outer surface tangential stress for a cylindrical shell.
  - SS-V: 1220 Displacements in Hemispherical Shell
    Test No. VS23 Find displacements in a hemispherical shell.
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SS-V: 1220 Displacements in Hemispherical Shell

Test No. VS23 Find displacements in a hemispherical shell.

Definition

Boundary Conditions
Point E: Zero displacement
Edge AE: Symmetry about ZX plane
Edge CE: Symmetry about YZ plane

All other displacements on edge AC are free. Concentrated radial loads of 2 KN outwards at A and inwards at C.

The material properties are:

Property: Value
Young's Modulus: 68.25e3 MPa
Poisson's Ratio: 0.3

Results

The following table summarizes the displacement results.


	Reference¹	SimSolid	% Difference
Displacement at A along x-axis	0.185 m	0.1859 m	~0.48

¹ Test LE3 from NAFEMS Publication NNB, Rev. 3, NAFEMS Linear Benchmarks, 5 Oct 1990