Nasa rotor 37 fluent density based solver
Hello guys .. im solving nasa rotor 37 single blade with rotationaly periodic boundary conditions .. i am using inlet and outlet pressure boundary condition .. the grid is 1.5 million .. the y plus is varying from 10 to 100 .. the problem is not converging at all .. i tried to reduce the cfl to 0.01 .. could someone help me with the problem!!!
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Hi
How did you set periodic boundary condition? maybe you set translational periodic. Regards |
no .. its rationally periodic with periodic angle 10 deg
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