Convergence Issue in Subsonic Aerodynamics Problem
I am currently running a simulation on Mach 0.6 with SA model. My residuals converge to 1e-3 for First Order scheme. But with second order scheme they don't go below 1e-2.
Whats the problem, whether its mesh or solver settings? What should I do to improve the convergence? |
All times are GMT -4. The time now is 02:01. |