NASA NTRS · 19930088436
Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 2.46 and 3.36
Abstract
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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Kaattari, George E. 1955-01-18. Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 2.46 and 3.36. https://ntrs.nasa.gov/citations/19930088436
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