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Physics, 12.08.2020 05:01 bm42400

Assume the angle of attack = 0. Use linear supersonic theory to determine Cp (x) on the upper and lower surfaces. Plot the pressure coefficient on the upper and lower surfaces and indicate on the plot what sectio

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Assume the angle of attack = 0. Use linear supersonic theory to determine Cp (x) on the upper and l...
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