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Altitude Performance and Operational Characteristics of 29-inch-diameter Tail-pipe Burner with Several Fuel Systems and Fuel-cooled Stage-type Flame Holders on J35-A-5 Turbojet Engine / Richard L. Golladay and Harry E. BloomerAn investigation of tail-pipe burning was conducted in the NACA Lewis altitude wind tunnel with a full-scale turbojet engine and an 29-inch-diameter tail-pipe burner. Effects of fuel distribution and number and arrangement of stages on performance and operational characteristics of several fuel-cooled flame holders are presented and discussed. Operation with a three-stage flame holder having the large stage upstream was the most efficient. Combustion efficiency was slightly increased at high altitudes by injecting fuel upstream of the flame holder.
Document ID
19930086171
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Golladay, Richard L
Bloomer, Harry E
Date Acquired
August 16, 2013
Publication Date
April 28, 1950
Report/Patent Number
NACA-RM-E50A19
Report Number: NACA-RM-E50A19
Accession Number
93R15461
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBINES, GAS - AFTERBURNING
ENGINES, TURBOJET

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