Effects of several leading-edge modifications on the stalling characteristics of a 45 degree swept-forward wing
Description:
Report presenting an investigation to determine the effects of several leading-edge modifications on the maximum lift and pitching-moment characteristics on a large-scale 45 degree swept-forward wing. A full-span leading-edge flap deflected 30 degrees down tended to give the largest gain of maximum lift. Results regarding the plain leading-edge flaps and cambered nose are explored.
Date:
June 14, 1949
Creator:
McCormack, Gerald M. & Cook, Woodrow L.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department