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EFFECT OF FUEL INJECTORS AND LINER DESIGN ON PERFORMANCE OF AN ANNULAR TURBOJET COMBUSTOR WITH VAPOR FUELEffect of fuel injector and liner design on performance of turbojet combustor with vapor fuel
Document ID
19630004000
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Childs, J. H. (NASA Lewis Research Center Cleveland, OH, United States)
Norgren, C. T. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2013
Publication Date
April 6, 1953
Subject Category
Physics, Solid-State
Report/Patent Number
NACA-RM-E53B04
Report Number: NACA-RM-E53B04
Accession Number
63N13876
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMBUSTOR
FUEL INJECTION
LINER

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