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Advanced technology for controlling pollutant emissions from supersonic cruise aircraftGas turbine engine combustor technology for the reduction of pollutant emissions is summarized. Variations of conventional combustion systems and advanced combustor concepts are discussed. Projected results from far term technology efforts aimed at applying the premixed prevaporized and catalytic combustion techniques to aircraft combustion systems indicate a potential for significant reductions in pollutant emission levels.
Document ID
19810009481
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Duerr, R. A. (NASA Lewis Research Center Cleveland, OH, United States)
Diehl, L. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1980
Publication Information
Publication: NASA. Langley Research Center Supersonic Cruise Res. 1979, Pt. 1
Subject Category
Environment Pollution
Accession Number
81N18004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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