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Incompressibe airfoil simulation
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Statistics
0Â Geometries
1Â Mesh
1Â Simulation setup
17Â Results
0Â Geometries 1Â Mesh 1Â Simulation setup 17Â ResultsAbout this project
How we can divide the domain into more number of cells , integration , linear equation system and finally solving by using different solvers . to find residual , relaxation factors , various numerrical schemes detrermine the stability and convergence rate . By changing the values of relaxation factor the execution time and clock time is varied. in this project run the simulation by various relaxation factor , GAMG , PCG , Smooth solvers .we get differnt results. at certain value of relaxation factor it diverges and some it will give good results of convergence rate .
