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Effect of fuel distribution and flame stabilization techniques on combustion stability limits for swirl-can combustor modules burning ASTM-A1 fuelEffect of fuel distribution and flame stabilization techniques on combustion stability limits for swirl-can combustor modules
Document ID
19710008249
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Briehl, D. C. (NASA Lewis Research Center Cleveland, OH, United States)
Ingebo, R. D. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
E-5968
NASA-TM-X-2185
Accession Number
71N17724
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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