Elements tested
- DC1D2
- DC1D3
- DC2D3
- DC2D4
- DC2D6
- DC2D8
- DCAX3
- DCAX4
- DCAX6
- DCAX8
- CAX3T
- CAX4RHT
- CAX4RT
- CAX4T
- CPE3T
- CPE4RHT
- CPE4RT
- CPE4T
- CPE6MHT
- CPE6MT
- CPS3T
- CPS4RT
- CPS4T
- CPS6MT
- C3D4T
- C3D6PHT
- C3D6PT
- C3D6T
- C3D8RHT
- C3D8RT
- C3D8T
- SC6RT
- SC8RT
- EC3D8RT
ProductsAbaqus/StandardAbaqus/Explicit Elements tested
Problem descriptionModel:The geometry is shown above. A uniform mesh with 10 elements along the length of the bar is used. The thickness and width of the bar are each 0.01 m. In Abaqus/Standard a steady-state simulation is performed, while in Abaqus/Explicit a transient simulation is performed. The total simulation time in the latter case is 2500 seconds. This provides enough time for the transient solution to reach steady-state conditions in this problem. Material:Conductivity = 55.6 W/m°C, specific heat = 460.0 J/kg°C, density = 7850 kg/m3. At end B emissivity = 0.98, Stefan-Boltzmann constant = 5.67 × 10−8 W m2/ K4. For the coupled temperature-displacement elements dummy mechanical properties are used to complete the material definition. Boundary conditions:Prescribed temperature of 1000 K at end A. Radiation to ambient temperature of 300 K at end B. No heat flux perpendicular to AB. Loading:Zero internal heat generation. Reference solutionThis is a test recommended by the National Agency for Finite Element Methods and Standards (U.K.): Test T2 from NAFEMS publication TNSB, Rev. 3, “The Standard NAFEMS Benchmarks,” October 1990. Target solution: Temperature at B=927 K (653.85°C). Results and discussionAll elements yield the exact solution. Input filesAbaqus/Standard input files
Abaqus/Explicit input files
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