Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 1.45 and 1.97

Kaattari, George E
naca-rm-a54d19
June 25, 1954


Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings of aspect ratios 2 and 4 at Mach numbers of 1.45 and 1.97. The investigation includes some comparison of the effects of Reynolds number and of thickening the wing root sections on the loading.

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