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タイトルLangley 8-Ft. HTT Test 139 Gas Analyses
本文(外部サイト)http://hdl.handle.net/2060/20000005107
著者(英)Sprinkle, Danny R.; Davis, Patricia P.
著者所属(英)NASA Langley Research Center
発行日1999-10-01
言語eng
内容記述This report presents results of gas analyses of Mach 7 Tunnel Calibration Test 139 conducted in the Langley 8-Ft. HTT from May through June of 1998. These tests in support of hypersonic airbreathing propulsion provided a current calibration at the primary test condition for the National Aero-Space Plane Concept Demonstration Engine and a new calibration for the two test conditions that will be used for engine testing in support of the Hyper-X program. Samples taken from three probes on the Flow Survey Apparatus were analyzed using mass spectrometers. Although this wind tunnel doesn't produce a true simulation of flight conditions, test results show that a uniform oxygen concentration of 21 percent was achieved.
NASA分類Chemistry and Materials (General)
レポートNONASA/TM-1999-209712
L-17766
NAS 1.15:209712
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/95500


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