Inverse Aerofoil Optimiser using CST, Python and Xfoil
I'm seeking an expert in aerodynamics and computational fluid dynamics to improve my existing inverted NACA4412 pressure distribution. Ideally, you will: - Have extensive experience working with CST, Python and Xfoil... (Budget: £20 - £250 GBP, Jobs: Aerospace Engineering, Engineering, Matlab and Mathematica, Mechanical Engineering, Python)
