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An airplane is flying at an altitude of 12,000 m. Determine the gauge pressure at the stagnation point on the nose of the plane

 

An airplane is flying at an altitude of 12,000 m. Determine the gauge pressure at the stagnation point on the nose of the plane if the speed of the plane is 200 km/h. Make necessary assumptions. Altitude 12,000 m 2 200 km/h

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