Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a Model of an 82 Deg Delta Wing Airplane Having Auxiliary Variable-sweep Wing Panels

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Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a Model of an 82 Deg Delta Wing Airplane Having Auxiliary Variable-sweep Wing Panels
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Total Pages : 44
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ISBN-10 : NASA:31769000463391
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