Question: Consider an infinitely thin flat plate at an angle of attack a in a Mach 2.6 flow. Calculate the lift and wave-drag coefficients for (a)

Consider an infinitely thin flat plate at an angle of attack a in a Mach 2.6 flow. Calculate the lift and wave-drag coefficients for

(a) α = 5°

(b) α = 15°

(c) α = 30°

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M P2 P3 a For M 26 and e 5 B 265 M M sinB 26 sin 265 116 M P3 P From Table A1 for M 26 From Table A2 ... View full answer

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