Question
3. The pressure at a point on the wing of an airplane is 7.58 X 10 N/m. The airplane is flying with a velocity
3. The pressure at a point on the wing of an airplane is 7.58 X 10 N/m. The airplane is flying with a velocity of 70 m/s at free stream density-1.23 kg/m, pressure =8.28x10 N/m. Calculate the pressure coefficient at this point of the wing.
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Conceptual Physics
Authors: Paul G. Hewitt
11th edition
321568095, 9780-032166256, 321662563, 978-0321568090
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