NACA research memorandum RM (series). L53D13. Effects of trailing-edge bluntness on lift, drag, and pitching-moment characteristics of unswept, 45° swept, and 45° delta wings at Mach numbers of 1.41, 1.62, and 1.96 [with list of references]; by Kennith L. Goln and Gertrude C. Westrick.

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