Question: 3 - Consider a half - diamond airfoil with a freestream Mach number of M = 3 . 7 , a wedge angle of =

3- Consider a half-diamond airfoil with a freestream Mach number of M=3.7, a wedge angle of =3.0, and an angle of attack of a =4.0. Compute the pressure ratio for each surface, the lift coefficient, and the drag coefficient use the shock/expansion method and linearized theory.
3 - Consider a half - diamond airfoil with a

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