NASA NTRS · 19710000030
Lift distribution in a rectangular jet
Abstract
Computer programs predict effect of slipstream-wing flow interaction on aerodynamic characteristics of deflected slipstream and tilt aircraft. One program calculates lift distribution, lift, and drag of wing in wide slipstream. Results permit development of simplified lifting surface theory for circular jet.
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Jameson, A.. 1971-02-01. Lift distribution in a rectangular jet. https://ntrs.nasa.gov/citations/19710000030
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