A computational procedure is developed, based on lifting line theory, which successfully predicts the spanwise lift distribution at moderate blowing momentum coefficient on a high aspect ratio (AR = 18) circulation control wing-body model with several variations in the spanwise lift distribution which validates this procedure. Additional keywords: Coanda surface; Wing body configurations; Mathematical models. (Author)
Lift Distribution on a High Aspect Ratio Circulation Control Wing with Root Lift Cutout
1985
53 pages
Report
Keine Angabe
Englisch
Solid State Physics , Aerodynamics , Lift , High lift , Mathematical prediction , Blowers , Coefficients , Momentum , Coanda effect , Surfaces , Aspect ratio , High rate , Theory , Circulation , Wing body configurations , Control , Computations , Distribution , Mathematical models , Circulation control wings , Lifting line theory
Unsteady lift of wing of finite aspect ratio
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