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WIND-TUNNEL INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF A MODEL REPRESENTATIVES OF A SUPERSONIC FIGHTER-CLASS AIRPLANE WITH AN EXTERNAL-FLOW JET-AUGMENTED FLAP IN LOW-SPEED FLIGHT [NASA TN D-50]

By: Newson, William A.
Material type: materialTypeLabelBookPublisher: Washington, D.C. National Aeronautics and Space Administration 1959Description: 84p.
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