validation of wind tunnel data
I have simulated the 3D airfoil in Fluent, and monitor lift and drag force for particular Reynolds number. My wing model dimension is in "mm" and finally my lift and drag force are in "256345" and -345728. is this possible. what are the factors should be consider. Is this lift force or lift coefficient. pls reply me.
|All times are GMT -4. The time now is 15:07.|