Boundary condition setting
i have run simulation on NACA 0012 airfoil by SW/cosmofloworks external flow and i noticed that difference boundary condition give different result (lift and drag coefficient vs AOA graph)...do i need to use the initial setting boundary condition or set it to wind tunnel test section?? and how to know that the setting is suitable or not?
|All times are GMT -4. The time now is 04:46.|