Five-component force data showing effects of applying boundary layer control to flaps of fighter aircraft and data defining air flow requirements of boundary layer control system; with nose flap deflected 45° substantial improvements in maximum lift, aileron effectiveness, and longitudinal stability are obtained.
Full-scale wind-tunnel tests of low-aspect-ratio, straight-wing airplane with blowing boundary-layer control on leading-and trailing-edge flaps
NASA -- Tech Note
1959
24 pages
Report
English
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