Effect of pressure level on afterburner-wall temperatures Metadata

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Title

  • Main Title Effect of pressure level on afterburner-wall temperatures
  • Series Title NACA Research Memorandums

Creator

  • Author: Shillito, Thomas B.
    Creator Type: Personal
  • Author: Smolak, George R.
    Creator Type: Personal

Contributor

  • Originator: Lewis Flight Propulsion Laboratory
    Contributor Type: Organization
    Contributor Info: NASA Lewis Research Center

Date

  • Creation: 1958-06-11

Language

  • English

Description

  • Content Description: Report presenting an investigation conducted on a full-scale afterburner and turbojet engine to determine the effect of pressure level on afterburner-wall temperature. For a given ratio of cooling airflow to afterburner gas flow, the afterburner-wall temperature increased as afterburner-outlet pressure was increased. The results indicated that heat transfer by luminous radiation was not significant any pressure level investigated.
  • Physical Description: 23 p. : ill.

Subject

  • Keyword: turbojet engines
  • Keyword: aircraft afterburners

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: 63N12515
  • URL: http://hdl.handle.net/2060/19630002639
  • Report No.: NACA-RM-E58D01
  • Center for AeroSpace Information Number: 19630002639
  • Archival Resource Key: ark:/67531/metadc52844