| Title: | Test No IC18 - Hemisphere Point Load |
| Image: | ![]() |
| Example Type: | NAFEMS Benchmark |
| Customer Name: | SOFiSTiK |
| SOFiSTiK Program: | ASE |
| Application Area: | Building Design Lightweight Structures |
| Description: | In this test the shell system, depicted above, is analysed with two point loads, each of 2 kN (acting towards the inside and outside respectively), whereby an isotropic material with an E-modulus of 68.25*10³ MPa and a poisson's ratio of 0.3 are used. The system is generated in such a manner, so as to allow the calculation of several different element meshes consisting of quad-elements. The following element meshes are investigated: 4x4 elements, 8x8 elements and 16x16 elements. The calculation is made with the program ASE. More precise description: NAFEMS: Linear Statics Benchmarks, Vol. 1 Results: x-displacement for point A. Theoretical value 0.185 m analytically. Benchmark value 0.1838 m (fine mesh, 8-node quad-element). Deviation of program ASE from the anlytical result in case of 4x4 elements 35.1 %, in case of 8x8 2.8 %, in case of 16x16 elements 0 %. Further results in the DAT-file. |
| Keywords: | NAFEMS, Benchmark, Shell, Point load, Symmetry conditions |
| Creation Date: | 08.09.2006 |
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