problem in fan boundary condition
hi CFD online team
i am working on a project of a small aircraft with a propeller.in order to cater the propeller effects i am using fan boundary conditions, and i have written a UDF, for profile specification of tangential velocity. my problem is the effect of fan is only visible of density based solver, and not for pressure based solver.where as my mach number is only .171 |
Regarding uDF
Assalamu alaikum Sis
I'm also working in UDF for Fan boundary condition for Wind Turbine. Can we do by discussing my email id is "er_ijaz@yahoo.com" |
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