High-pressure blowing over flap and wing leading edge of a thin large-scale 49 degree swept wing-body-tail configuration in combination with a drooped nose and a nose with a radius increase
Description: From Summary: "A 49 degree swept-wing complete model equipped for high-pressure blowing full span at two chordwise locations at the leading edge of a full-span wing and over a half-span flap has been tested in the Langley full-scale tunnel to determine the effectiveness of blowing at the leading edge as a supplementary leading-edge stall control at high lift coefficients." The effect of blowing on the lift characteristics, pitching-moment characteristics, and drag characteristics of this particular model is described.
Date: May 28, 1957
Creator: Fink, Marvin P. & McLemore, H. Clyde
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department