Consider an infinitely thin flat plate of chord cat an angle of attack d-5 surfaces are different and given as, P= 35(x/c-x/d kPa and p) =0.56 (x/) kPa. Ignoring the shear stress, calculate the location of the center of pressure. (Round the final answer to two decimal place) The location of the center of pressure, Xcp C.
Consider an infinitely thin flat plate of chord cat an angle of attack d-5 surfaces are different and given as, P= 35(x/c-x/d kPa and p) =0.56 (x/) kPa. Ignoring the shear stress, calculate the location of the center of pressure. (Round the final answer to two decimal place) The location of the center of pressure, Xcp C.
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Transcribed Image Text:Consider an infinitely thin flat plate of chord cat an angle of attack a=5°in a subsonic flow. The pressures on the upper and lower
surfaces are different and given as, px) = 3.5(x/(1-x/c) kPa and px) =0.56 (x/) kPa. Ignoring the shear stress, calculate the location
of the center of pressure (Round the final answer to two decimal place)
The location of the center of pressure, Xep
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