Title: Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 1.45 and 1.97
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 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.
Publication Year: 1954
Publication Date: 1954-06-25
Language: en
Type: article
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Cited By Count: 4
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