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An airplane is flying northeast toward New York at a velocity of 60 m/s and a standard altitude of 3km. Sensors on the wing have deterined that the airflow over a specific point on the wing has a velocity of 70m/s. If the flow is incompressible for this condition. Calculate the pressure at the point were the velocity was determined to be 70m/s
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The expert examines aerodynamics of an airplane flying northeast towards New York at a given velocity.
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If we assume an incompressible, irrotational, inviscid, and steady flow, then we can use Bernoulli's equation: ...
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