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Afterburner performance of film-vaporizing V-gutters for inlet temperatures up to 1255 KCombustion tests of five variations of an integral, spray-bar - flameholder combination were conducted in a 0.49-m-diameter duct. Emphasis was on low levels of augmentation. Fuel impinged on guide plates, mixed with a controlled amount of inlet air, vaporized, and was guided into the V-gutter wake. Combustor length was 0.92 m. Good performance was demonstrated at fuel-air ratios less than 0.025 for inlet temperatures of 920 to 1255 K. Maximum combustion efficiency occured in the vicinity of fuel-air ratios of 0.02 and was 92 to 100 percent, depending on the inlet temperature. Lean blowout fuel-air ratios were in the vicinity of 0.005. Improvements in rich-limit blowout resulted from enlarging the guide-flow passageway areas. Other means of extending the operating range are suggested. A simplified afterburner concept for application to advanced engines is described.
Document ID
19730020187
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Branstetter, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Reck, G. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1973
Subject Category
Thermodynamics And Combustion
Report/Patent Number
E-7435
NASA-TM-X-2855
Report Number: E-7435
Report Number: NASA-TM-X-2855
Accession Number
73N28919
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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