Question: Consider a flat plat at = 20o in Mach 20 free stream. Using straight Newtonian theory, calculate the lift and wave-draw coefficients. Compare these

Consider a flat plat at α = 20o in Mach 20 free stream. Using straight Newtonian theory, calculate the lift and wave-draw coefficients. Compare these results with exact shock-expansion theory.

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M 20 P P3 From Newtonian theory C 2 sin2 2 sin 20 0234 Cp 02... View full answer

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