Preliminary experimental investigation of transpiration cooling for an afterburner with a sintered, porous stainless-steel combustion-chamber wall Metadata

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Title

  • Main Title Preliminary experimental investigation of transpiration cooling for an afterburner with a sintered, porous stainless-steel combustion-chamber wall
  • Series Title NACA Research Memorandums

Creator

  • Author: Koffel, William K.
    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: 1953-06-08

Language

  • English

Description

  • Content Description: Report presenting an experimental investigation of the application of transpiration air-cooling to the combustion-chamber wall of an afterburner. Results regarding the typical temperature and pressure profiles, correlation of wall temperatures, distribution of cooling-air flux density, longitudinal distribution of cooling air, longitudinal distribution of wall temperature, effect of permeability on cooling-air requirements, and fabricating and operating problems are provided.
  • Physical Description: 47 p. : ill.

Subject

  • Keyword: aircraft afterburners
  • Keyword: transpiration cooling

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: 93R17099
  • URL: http://hdl.handle.net/2060/19930087809
  • Report No.: NACA-RM-E53D08
  • Center for AeroSpace Information Number: 19930087809
  • Archival Resource Key: ark:/67531/metadc59787