NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Fuel Vaporization EffectsA study of the effects of fuel-air preparation characteristics on combustor performance and emissions at temperature and pressure ranges representative of actual gas turbine combustors is discussed. The effect of flameholding devices on the vaporization process and NOx formation is discussed. Flameholder blockage and geometry are some of the elements that affect the recirculation zone characteristics and subsequently alter combustion stability, emissions and performance. A water cooled combustor is used as the test rig. Preheated air and Jet A fuel are mixed at the entrance of the apparatus. A vaporization probe is used to determine percentage of vaporization and a gas sample probe to determine concentration of emissions in the exhaust gases. The experimental design is presented and experimental expected results are discussed.
Document ID
19830020943
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bosque, M. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1983
Publication Information
Publication: Combust. Fundamentals Res.
Subject Category
Propellants And Fuels
Accession Number
83N29214
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available