Engineering, 15.04.2020 20:48 twinkle713derp
Consider an infinitely thin flat plate of chord c at an angle of attack α in a supersonic flow. The pressure on the upper and lower surfaces are different but constant over each surface; that is, pu(s) = C1 and pl(s) = C2, where C1 and C2 are constants and C2 > C1. Ignoring the shear stress, calculate the location of the center of pressure.
Answers: 3
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Consider an infinitely thin flat plate of chord c at an angle of attack α in a supersonic flow. The...
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