Consider an infinitely thin flat plate of chord c at an angle of attack in a supersonic flow.The pressures on the upper and lower surfaces are different but constant over each surface;that is, ????????(????) = ????1 and ????????(????) = ????2, where ????1 and ????2 are constants and ????2 > ????1. Ignoring theshear stress, calculate the location of the center of pressure.