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

Kaattari, George E
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.

An Adobe Acrobat (PDF) file of the entire report: