Nasa rotor 37 fluent density based solver

sehs15 · April 30, 2014, 11:14

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!!!

CFD-fellow · May 1, 2014, 13:27

Hi
How did you set periodic boundary condition? maybe you set translational periodic.
Regards

sehs15 · May 2, 2014, 07:12

no .. its rationally periodic with periodic angle 10 deg

April 30, 2014, 11:14	Nasa rotor 37 fluent density based solver	#1
sehs15 New Member mohamed mohsen Join Date: Oct 2012 Posts: 29 Rep Power: 13	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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May 1, 2014, 13:27		#2
CFD-fellow Senior Member Behrooz Jamshidi Join Date: Apr 2013 Posts: 110 Rep Power: 13	Hi How did you set periodic boundary condition? maybe you set translational periodic. Regards

May 2, 2014, 07:12		#3
sehs15 New Member mohamed mohsen Join Date: Oct 2012 Posts: 29 Rep Power: 13	no .. its rationally periodic with periodic angle 10 deg