4-1. Exact solution
A slender airfoil with sharp leading edge in Mach = 1 flow
Results using Rheoelectric analogy to basic equations and verification with an Analog Computer
Transonic test case for numerical analysis codes
Analytical results for airfoil shape, camber/thickness ratio, flow angle of attack |
Parabolic pressure distribution for cusped airfoil in sonic freestream. |
Lift and drag for cusped airfoils with various camber/thickness ratio |
Mach number distribution for cusped airfoil in sonic flow MACH = 1, (CFD analysis) |
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