Title: Investigation of high-angle-of-attack performance of a 14 deg ramp-type inlet in various circumferential body locations, Mach number range 1.5 to 2.0
Abstract: Internal flow performance of fixed 14 deg ramp inlet from zero to 20 deg angle of attack at supersonic free stream
Publication Year: 1957
Publication Date: 1957-06-26
Language: en
Type: article
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Cited By Count: 1
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