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Effects of fuel-nozzle carbon deposition on combustion efficiency of single tubular-type, reverse-flow turbojet combustor at simulated altitude conditions

Ralph T Dittrich

Abstract

Report presenting an investigation to study the effects of changes in fuel-nozzle carbon deposition on the combustion efficiency of a single tubular-type, reverse-flow, turbojet combustor. The investigation was conducted because of the need to improve the reproducibility of combustion data for fuel-research purposes.

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Available abstract

Key concepts: Combustor, Nozzle, Combustion, Turbojet, Deposition (geology), Flow (mathematics), Carbon fibers, Combustion chamber