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Pressesc to exit full screen A flying-wing bomber is cruising at 15,000 meters. The wing can be approximated by a flat plate with a
Pressesc to exit full screen A flying-wing bomber is cruising at 15,000 meters. The wing can be approximated by a flat plate with a 2.5-meter chord and 35-meter span. If the angle of attack is 2, what is the approximate lift coefficient and wave-drag coefficient if the craft is cruising at M = 1.2? What are the lift and wave-drag forces acting on the wing? Solve the problem in the International system of units. ZOOM +
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