Effect of hot-gas bleedback ice prevention on performance of a turbojet engine with fixed-area tail-pipe nozzle Metadata

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Title

  • Main Title Effect of hot-gas bleedback ice prevention on performance of a turbojet engine with fixed-area tail-pipe nozzle
  • Series Title NACA Research Memorandums

Creator

  • Author: Dietz, Robert O., Jr.
    Creator Type: Personal
  • Author: Krebs, Richard P.
    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: 1949-05-16

Language

  • English

Description

  • Content Description: Report presenting the results of an analytical investigation, which demonstrated that the inlet of a turbojet engine can be protected from ice accretions by bleeding hot gases from other locations within the engine to the inlet without undue loss in thrust. Results regarding the bleedback requirements, engine performance, effect of nozzle area, mixing efficiency, and seriousness of thrust losses are provided.
  • Physical Description: [26] p.

Subject

  • Keyword: turbojet engines
  • Keyword: ice prevention
  • Keyword: gas bleedback

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: 93R15266
  • URL: http://hdl.handle.net/2060/19930085976
  • Report No.: NACA-RM-E9B23
  • Center for AeroSpace Information Number: 19930085976
  • Archival Resource Key: ark:/67531/metadc58308