Steady Loads Due to Jet Interference on Wings, Tails, and Fuselages at Transonic Speeds


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This paper gives the results of some recent investigations of jet-interference effects on actual airplane configurations at transonic speeds. Data presented herein were obtained with hot jets on both wind-tunnel and flight models. Results indicate that jet-induced effects are small at subsonic speeds; however, at low supersonic Mach numbers, these effects are comparable to those obtained at substantially higher Mach numbers.







NASA Technical Note


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