1953•Unpublished venueRequires access

Performance of an Annular Turbojet Combustor Having Reduced Pressure Losses and Using Propane Fuel

C. T. Norgren, J Howard Childs

Abstract

Report presenting an investigation to develop a high-combustion-efficiency turbojet combustor with pressure losses typical of those encountered in current turbojet engines. A total of 13 air-entry hole modifications was investigated to obtain a combustor design with high combustion efficiencies and a satisfactory outlet radial temperature profile. Results regarding combustor development and the performance of Model 28I are provided.

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Key concepts: Combustor, Turbojet, Combustion, Combustion chamber, Automotive engineering, Aerospace engineering, Propane, Engineering