Lift and pitching-moment interference between a pointed cylindrical body and triangular wings of various aspect ratios at Mach numbers of 1.50 and 2.02

Jack N. Nielsen, Elliott D. Katzen, Kenneth K. Tang
Sep 1950

In order to investigate the effects of interference on wing-body combinations, tests were conducted at Mach numbers of 1.50 and 2.02 of a pointed, cylindrical body, of six triangular wings having aspect ratios from 0.67 to 4.00, and of the wings and the body in combination.

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