I'm currently trying to design a more efficient 2 blade propeller for a quadcopter and I'm new to the Caeses platform. What would be the most efficient way to design a new 2 blade propeller, by changing the chord, NACA, etc under certain conditions (RPM, velocity, flight angle)?
I don't have CFD software on my personal computer if that's the best route to take. Is it possible to download it on my schools computer that has ANSYS?
Thank you very much,