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Spectral flame radiance from a tubular-can combustorAn experimental investigation was conducted to determine the effects of fuel type, fuel-air ratio, and inlet-air pressure on the spectral flame radiance emanating from a JT8D can combustor. Spectral radiance measurements from 1.55 to 5.5 micrometers of wavelength were recorded and analyzed to determine soot concentration and flame temperature at various axial locations in the combustor. Two fuels differing in volatility, viscosity, and chemical composition were used in this investigation.
Document ID
19810010595
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Claus, R. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TP-1722
E-509
Report Number: NASA-TP-1722
Report Number: E-509
Accession Number
81N19121
Funding Number(s)
PROJECT: RTOP 505-32-32
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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