Research program on low-speed aerodynamics as applied to STOL and VTOL aircraft conducted by Cornell Aeronautical Laboratory; paper presents experimental data on airfoil maximum lift in 2-dimensional shear stream and theoretical studies devoted to explaining these results; experimental data showing destalling phenomena are discussed, and results of theoretical studies presented to illustrate effects of shear on airfoil stall.
Influence of two-dimensional stream shear on airfoil maximum lift
J Aerospace Sciences
Journal of the Aero/Space Sciences ; 29 , n 8 ; p 889-904
1962
16 pages
Aufsatz (Zeitschrift)
Englisch
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