Preliminary investigation of the flow in an annular-diffuser-tailpipe combination with an abrupt area expansion and suction, injection, and vortex-generator flow controls Metadata

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Title

  • Main Title Preliminary investigation of the flow in an annular-diffuser-tailpipe combination with an abrupt area expansion and suction, injection, and vortex-generator flow controls
  • Series Title NACA Research Memorandums

Creator

  • Author: Henry, John R.
    Creator Type: Personal
  • Author: Wilbur, Stafford W.
    Creator Type: Personal

Contributor

  • Originator: Langley Aeronautical Laboratory
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab

Date

  • Creation: 1954-02-10

Language

  • English

Description

  • Content Description: Report presenting an investigation of the performance of an annular-diffuser-tailpipe combination with an abrupt area expansion with and without flow controls in the form of suction, injection, and vortex generators. Results regarding the inlet measurements, longitudinal static-pressure distribution, radial distributions, and mean performance coefficients are provided.

Subject

  • Keyword: annular-diffuser-tailpipe combinations
  • 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: 93R17277
  • URL: http://hdl.handle.net/2060/19930087987
  • Report No.: NACA-RM-L53K30
  • Center for AeroSpace Information Number: 19930087987
  • Archival Resource Key: ark:/67531/metadc59931