Engineering, 13.11.2019 00:31 stodd9503
Consider a wing in a high-speed wind tunnel. at a point on the wing, the velocity is 850 ft/s. if the test-section fl ow is at a velocity of 780 ft/s, with a pressure and temperature of 1 atm and 505°r, respectively, calculate the pressure coeffi cient at the point.
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Consider a wing in a high-speed wind tunnel. at a point on the wing, the velocity is 850 ft/s. if th...
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