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タイトルJet Effects on Base and Afterbody Pressures of a Cylindrical Afterbody at Transonic Speeds
本文(外部サイト)http://hdl.handle.net/2060/19930089150
著者(英)Cubbage, James M , Jr
著者所属(英)National Advisory Committee for Aeronautics. Langley Aeronautical Lab.
発行日1956-05-23
言語eng
内容記述An investigation of the effects of jet nozzle geometry, size of base annulus, and base bleed upon the base and afterbody pressures of a cylindrical afterbody at transonic speeds has been conducted. Sonic and supersonic conical nozzles with jet-to-base diameter ratios from 0.25 to 0.85 were investigated with a cold jet at jet total-pressure ratios up to approximately 8.0 through a Mach number range from 0.6 to 1.25. Base pressure coefficients of about -0.55 were measured for the sonic nozzles at a Mach number of 1 or greater. The jet-to-base diameter ratio had a substantial effect on the base pressure obtained on the cylindrical afterbody of this investigation. Base bleed was beneficial in increasing the base pressure under certain conditions but had little or no effect at certain other conditions.
レポートNO93R18440
NACA-RM-L56C21
権利No Copyright


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