Effects of trailing-edge bluntness on the lift, drag, and pitching-moment characteristics of unswept, 45 degree swept, and 45 degree delta wings at Mach numbers of 1.41, 1.62, and 1.96

Goin, Kennith L Westrick, Gertrude C
naca-rm-l53d13
June 10, 1953


No Abstract Available

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