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

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Title

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

Creator

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

Contributor

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

Date

  • Creation: 1953-09-24

Language

  • English

Description

  • 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.

Subject

  • Keyword: aircraft combustors
  • Keyword: aircraft power

Collection

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

Institution

  • Name: UNT Libraries Government Documents Department
    Code: UNTGD

Rights

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

Resource Type

  • Report

Format

  • Text

Identifier

  • Accession or Local Control No: 93R17067
  • URL: http://hdl.handle.net/2060/19930087777
  • Report No.: NACA-RM-E53G24
  • Center for AeroSpace Information Number: 19930087777
  • Archival Resource Key: ark:/67531/metadc59759