Hi, I have ran a simulation with my plane model and all the coeficents seems to be incorrect except for the lift coefficient. I know for sure the drag coefficient isn’t 0.18 and the moment coefficient isn’t more than 0.01. I dont know why this is happening can you please help me.
Thank you so much for your time and effort,
Frank lucci
Hi Frank, thank you for using the forum
There could be many reasons why the results are not expected, but in order to acknowledge them, I will need to check your setup. Is it possible that you send the link please?
Also, what are your expectations regarding the results?