NDLI: Flame radiation

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Flame radiation

Content Provider	NASA Technical Reports Server (NTRS)
Author	Wear, J. D.
Copyright Year	1984
Description	Total radiation and heat flux data was obtained on a combustor liner by advanced instrumentation. If the results obtained by the special instrumentation are considered to be representative of the total radiation and heat flux, then the effect of variation of engine operating parameters and of fuel type can be more easily obtained. The special instrumentation used for these investigations consisted of five total radiometers and two total heat flux gages. The radiometers were arranged axially and circumferentially through sliding air seals in the outer liner. The two heat flux gages were welded in the outer liner between two circumferential radiometers. Static pressures were obtained on both the cold and the hot side of the outer liner in the area of the heat flux gages. Liner metal temperatures were also obtained. The combustor inlet pressure was varied over a nominal range of 0.5 to 2.07 MPa, inlet air temperature from 550 to 670 K, and fuel-air ratio from about 0.015 to 0.040. The two fuels tested were ASTM Jet A and a fuel designated as ERBS V. Results of the tests are discussed.
File Size	1831280
Page Count	10
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19870001771
Archival Resource Key	ark:/13960/t3615vz13
Language	English
Publisher Date	1984-10-01
Access Restriction	Open
Subject Keyword	Inorganic And Physical Chemistry Radiometers Inlet Pressure Pressure Measurement Fuel Injection Combustion Chambers Flame Propagation Jet Engine Fuels Fuel-air Ratio Heat Flux Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Article

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