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Engineering, 17.02.2020 21:31 barbiegirllover

The wing area of the Lockheed F-104 straight-wing supersonic fighter is approximately 210 ft. If the airplane weighs 16,000 lb and is flying in level flight at Mach 2.2 at a standard altitude of 36,000 ft, estimate the wave drag on the wings.

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The wing area of the Lockheed F-104 straight-wing supersonic fighter is approximately 210 ft. If the...
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