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Propulsion-Induced Aerodynamic Effects Measured with a 13.5% HSCT Model (1996)
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Aeroacoustics, Aerodynamic, Effects, Engine, High-Lift, High-Speed, HSCT, Induced, Measured, Model, Program, Propulsion, Research, Technology, Workshop
Smith, B.E., "Propulsion-Induced Aerodynamic Effects Measured with a 13.5% HSCT Model", High-Speed Research Program High-Lift Engine Aeroacoustics Technology Workshop, NASA Ames Research Center, March 5-7, 1996.
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