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Effect of increased fuel temperature on emissions of oxides of nitrogen from a gas turbine combustor burning ASTM jet-A fuelAn annular gas turbine combustor was tested with heated ASTM Jet-A fuel to determine the effect of increased fuel temperature on the formation of oxides of nitrogen. Fuel temperature ranged from ambient to 700 K. The NOx emission index increased at a rate of 6 percent per 100 K increase in fuel temperature.
Document ID
19740007546
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Marchionna, N. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Thermodynamics And Combustion
Report/Patent Number
E-7634
NASA-TM-X-2931
Report Number: E-7634
Report Number: NASA-TM-X-2931
Accession Number
74N15659
Funding Number(s)
PROJECT: RTOP 501-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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