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Approximate solutions of range for constant altitude – constant high subsonic speed flight of transport aircraft

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2004-05-13

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Cruise, Aerospace engineering, Mach number, Constant (computer programming), Range (aeronautics), Fuel efficiency, Aerodynamics, Turbojet, Altitude (triangle), Wing, Aircraft flight mechanics, Control theory (sociology), Physics, Computer science, Engineering, Mathematics, Geometry

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https://hdl.handle.net/11421/4429
 https://doi.org/10.1016/j.ast.2004.04.002

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