Incompressibe airfoil simulation

About 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 .