SUBAERF program developed for aerodynamic analysis and design of lowspeed wing-flap systems. SUBAERF based on linearized theory lifting-surface solution. Low speed aerodynamic analysis method used in SUBAERF provides estimates of wing performance which include effects of attainable leading edge thrust and vortex lift.
Aerodynamic Analysis of Low-Speed Wing-Flap Systems
NASA Tech Briefs ; 8 , 3
01.01.1985
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Englisch