Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 2.46 and 3.36

Kaattari, George E
naca-rm-a54j12
January 18, 1955


Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings of aspect ratios 2 and 4 at Mach numbers of 2.46 and 3.36. The investigation includes some comparison of the effects of Mach number, Reynolds number, and thickening the wing root sections on the loading.

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