HAWT blade design!
 

Hey,

I am trying to perform a validation study to a HAWT using CFD. The problem is that there aren't any information regarding the chord and twist angle to put into my code and validate. However, there is information about the power curve, airfoil types, hub and tip radius. I would like to design a blade with the same input to match the power curve. I need someone who knows how to reverse and design this blade.

Thanks in advance,

CFD help
 

I have experience with this kind of work. I did airfoil validation as a TA at my university, and I'm currently working at an aerospace/defense company doing aerodynamics on aircraft turbines and generators. Let me know if you still need assistant with this project.