Performance of an annular turbojet combustor having reduced pressure losses and using propane fuel Metadata

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  • Main Title Performance of an annular turbojet combustor having reduced pressure losses and using propane fuel
  • Series Title NACA Research Memorandums


  • Author: Norgren, Carl T.
    Creator Type: Personal
  • Author: Childs, J. Howard
    Creator Type: Personal


  • Originator: Lewis Flight Propulsion Laboratory
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab


  • Creation: 1953-09-24


  • English


  • Content Description: 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.
  • Physical Description: 38 p. : ill.


  • Keyword: aircraft combustors
  • Keyword: aircraft power


  • Name: National Advisory Committee for Aeronautics Collection
    Code: NACA
  • Name: Technical Report Archive and Image Library
    Code: TRAIL


  • Name: UNT Libraries Government Documents Department
    Code: UNTGD


  • Rights Access: public
  • Rights License: pd
  • Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available

Resource Type

  • Report


  • Text


  • Accession or Local Control No: 93R17067
  • URL:
  • Report No.: NACA-RM-E53G24
  • Center for AeroSpace Information Number: 19930087777
  • Archival Resource Key: ark:/67531/metadc59759