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Nonequilibrium combustion effects in supersonic streamsThis research program is a theoretical and experimental investigation of the effect of nonequilibrium conditions upon the performance of combustors employing supersonic flows. Calculations and experiments are made regarding the effects on the ignition of hydrogen of the nonequilibrium species (free radicals, atoms, water vapor, etc.) obtained using vitiated air. Results of this investigation show that the nonequilibrium free-radical content from a supersonic vitiated air source will cause early ignition of the hydrogen. An analysis of heated air expended from a high temperature source to test section conditions also indicates that there is sufficient free radical content in the incoming flow to cause early ignition. Water vapor, an inherent contaminant in the generation of vitiated air, was found to reduce the ignition delay period under the experimental conditions considered.
Document ID
19730003242
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jensen, R. M.
(Purdue Univ. West Lafayette, IN, United States)
Bryce, C. A.
(Purdue Univ. West Lafayette, IN, United States)
Reese, B. A.
(Purdue Univ. West Lafayette, IN, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1972
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-120932
Report Number: NASA-CR-120932
Accession Number
73N11969
Funding Number(s)
CONTRACT_GRANT: NGR-15-005-013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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