An airplane is flying through the air at 280 mph at an altitude of 8,000 ft. Assuming standard atmospheric conditions, what is the pressure at the leading edge of the wing at a point where the relative fluid velocity is zero (stagnation point)?
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An airplane is flying through the air at 280 mph at an altitude of 8,000 ft. Assuming standard atmospheric conditions, what is the pressure at the leading edge of the wing at a point where the relative fluid velocity is zero (stagnation point)?
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