Engineering, 20.01.2020 17:31 proxydayz
Consider an airplane flying with a velocity of 40 m/s in conditions identical to those at an altitude of 5 km in the standard atmosphere. at a point on the wing, the airflow velocity is 70 m/s. calculate the pressure at this point. assume inviscid, incompressible flow and the u. s. standard atmosphere is the relevant atmospheric model.
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Consider an airplane flying with a velocity of 40 m/s in conditions identical to those at an altitud...
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