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Consider an infinitely thin flat plate of chord c at 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/Xt-x/) KPa and p(x) -0.56 (x/c) 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 c at 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/Xt-x/) KPa and p(x) -0.56 (x/c) 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.

College Physics
College Physics
11th Edition
ISBN:9781305952300
Author:Raymond A. Serway, Chris Vuille
Publisher:Raymond A. Serway, Chris Vuille
Chapter1: Units, Trigonometry. And Vectors
Section: Chapter Questions
Problem 1CQ: Estimate the order of magnitude of the length, in meters, of each of the following; (a) a mouse, (b)...
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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
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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