







Hey guys, critique my airfoil CFD results
I am a 2nd year mechanical engineering student, I want to get better at ansys i.e.analyses and simulations
If you could provide me with sources to learn more from, then that would be very helpful full
I also have animation videos of it but for some reason I am unable to upload them together with images
Edit: From the comments I understood that I should have plotted for the coefficient of lift and drag not just the force. And this geometry has 0° angle of attack, it was provided to us by the faculty. The domain is small because I was told so to make it this size. I learnt today that it should be 10x
Again thank you for the comments