ProductsAbaqus/StandardAbaqus/Explicit Elements testedCPS3 CPS4 CPS4I CPS4R CPS6 CPS6M CPS8 CPS8R Problem descriptionModel:Plane stress problem with shape defined by ABCD. Functions defining the curves BC and AD are given above. Mesh:A coarse and a fine mesh are tested for each element. In addition, a very fine mesh is tested for each element in the explicit dynamic analysis. Material:Linear elastic, Young's modulus = 210 GPa, Poisson's ratio = 0.3, density = 7800 kg/m3. Boundary conditions:along edge AB, along edge CD. Loading:Uniform outward pressure of 10 MPa at outer edge BC. In the explicit dynamic analysis the loading is applied such that a quasi-static solution is obtained. Reference solutionThis is a test recommended by the National Agency for Finite Element Methods and Standards (U.K.): Test LE1 from NAFEMS publication TNSB, Rev. 3, “The Standard NAFEMS Benchmarks,” October 1990. Target solution: Tangential edge stress () at D is 92.7 MPa. Results and discussionThe results are shown in Table 1 and Table 2. The values enclosed in parentheses are percentage differences with respect to the reference solution.
*A comparison of the results for reduced-integration and full-integration lower-order elements indicates that the full-integration elements perform significantly better for problems with stress concentrations of this type.
Input filesAbaqus/Standard input filesCoarse mesh tests:
Abaqus/Explicit input filesCoarse mesh tests:
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