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The shock angle on front of the leading edge of a F-16 supersonic plane is 10 deg. The airplane speed is 4200 ft./sec. compose the
The shock angle on front of the leading edge of a F-16 supersonic plane is 10 deg. The airplane speed is 4200 ft./sec. compose the equation to compute the Mach number in terms of the shock angle and compute the Mach number.
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Product Marketing Management
Authors: Suat Ozsoy
1st Edition
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