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Advanced physics Problem 0703. For the supersonic flow over a diamond wedge as shown below. Prandtl-Meyer expansion wave 1 3 M,>1 oblique shock Given: M1=2.5,
Advanced physics
Problem 0703. For the supersonic flow over a diamond wedge as shown below. Prandtl-Meyer expansion wave 1 3 M,>1 oblique shock Given: M1=2.5, AOA=50, t/c=0.1 (t is the maximum thickness of the airfoil, c is the chord). Find c and Ca based on the Shock-Expansion TheoryStep by Step Solution
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