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Preliminary tests of a gas turbine combustor with an air atomizing fuel injector systemFeasibility and performance of air atomizing fuel injector in turbojet combustor
Document ID
19690031365
Document Type
Technical Memorandum (TM)
Authors
Bigelow, J. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 7, 1969
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-52688
Accession Number
69N40754
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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