Experimental investigation of hot-gas bleedback for ice protection of turbojet engines 2: nacelle with long straight air inlet Metadata

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Title

  • Main Title Experimental investigation of hot-gas bleedback for ice protection of turbojet engines 2: nacelle with long straight air inlet
  • Series Title NACA Research Memorandums

Creator

  • Author: Callaghan, Edmund E.
    Creator Type: Personal
  • Author: Ruggeri, Robert S.
    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: 1949-05-26

Language

  • English

Description

  • Content Description: Report presenting aerodynamic and icing investigations conducted in the icing research tunnel on a model of a turbojet-engine nacelle with a long straight air inlet in order to provide basic design criteria for hot-gas blowback systems. The most uniform temperature distribution was obtained with a bleedback of 4.4 percent at a gas temperature of 1000 degrees Fahrenheit and resulted in an average dry-air-temperature rise of 46 degrees Fahrenheit.
  • Physical Description: 34 p. : ill.

Subject

  • Keyword: aerodynamics
  • Keyword: icing investigations
  • Keyword: hot-gas blowback systems

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: 93R15202
  • URL: http://hdl.handle.net/2060/19930085912
  • Report No.: NACA-RM-E9C16
  • Center for AeroSpace Information Number: 19930085912
  • Archival Resource Key: ark:/67531/metadc58253

Note

  • Display Note: "II."