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タイトルBasic flow characteristics of a linear aerospike nozzle segment.
著者(英)Mueller, T. J.; Sule, W. P.
発行日1972-11-01
言語eng
内容記述The separated base flow region within a linear aerospike nozzle segment is investigated experimentally in an ejector-diffuser system. The nozzle-diffuser system and base pressure characteristics are described over the pressure ratio range from the 'open wake' to the 'closed wake' operation. Schlieren photographs and static pressure distributions along the test section centerline and top contour describe the transition from 'open wake' to 'closed wake' flow fields. Base pressure and static pressure distributions are utilized to present the effects of a ramp diffuser. The effects of base bleed on the base pressure ratio and structure of the nozzle flow field are also presented.
NASA分類AERODYNAMICS
レポートNO73A15908
ASME PAPER 72-WA/AERO-2
権利Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/459174


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