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Mass spectrometric gas composition measurements associated with jet interaction tests in a high-enthalpy wind tunnelKnowledge of test gas composition is important in wind-tunnel experiments measuring aerothermodynamic interactions. This paper describes measurements made by sampling the top of the test section during runs of the Langley 7-Inch High-Temperature Tunnel. The tests were conducted to determine the mixing of gas injected from a flat-plate model into a combustion-heated hypervelocity test stream and to monitor the CO2 produced in the combustion. The Mass Spectrometric (MS) measurements yield the mole fraction of N2 or He and CO2 reaching the sample inlets. The data obtained for several tunnel run conditions are related to the pressures measured in the tunnel test section and at the MS ionizer inlet. The apparent distributions of injected gas species and tunnel gas (CO2) are discussed relative to the sampling techniques. The measurements provided significant real-time data for the distribution of injected gases in the test section. The jet N2 diffused readily from the test stream, but the jet He was mostly entrained. The amounts of CO2 and Ar diffusing upward in the test section for several run conditions indicated the variability of the combustion-gas test-stream composition.
Document ID
19860015957
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lewis, B. W.
(NASA Langley Research Center Hampton, VA, United States)
Brown, K. G.
(Old Dominion Univ. Norfolk, Va., United States)
Wood, G. M., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Puster, R. L.
(NASA Langley Research Center Hampton, VA, United States)
Paulin, P. A.
(NASA Langley Research Center Hampton, VA, United States)
Fishel, C. E.
(NASA Langley Research Center Hampton, VA, United States)
Ellerbe, D. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1986
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
NASA-TM-87642
NAS 1.15:87642
L-16074
Report Number: NASA-TM-87642
Report Number: NAS 1.15:87642
Report Number: L-16074
Accession Number
86N25429
Funding Number(s)
PROJECT: RTOP 506-51-13-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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