Applications of auxiliary air injectors to supersonic wind tunnels Metadata

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Title

  • Main Title Applications of auxiliary air injectors to supersonic wind tunnels
  • Series Title NACA Research Memorandums

Creator

  • Author: Spiegel, Joseph M.
    Creator Type: Personal
  • Author: Hofstetter, Robert U.
    Creator Type: Personal
  • Author: Kuehn, Donald M.
    Creator Type: Personal

Contributor

  • Originator: Ames Aeronautical Laboratory (U.S.)
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Ames Aeronautical Lab

Date

  • Creation: 1953-11-25

Language

  • English

Description

  • Content Description: Report presenting a discussion of the adverse effects of high compression ratio requirements for supersonic wind tunnels as well as the use of second throats for alleviating those effects. The results indicated that an auxiliary air-injector system can reduce starting and running compression ratios as compared to a conventional wind tunnel with a divergent diffuser.
  • Physical Description: 53 p. : ill.

Subject

  • Keyword: wind tunnel testing
  • Keyword: air-injector 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: 93R17542
  • URL: http://hdl.handle.net/2060/19930088252
  • Report No.: NACA-RM-A53I01
  • Center for AeroSpace Information Number: 19930088252
  • Archival Resource Key: ark:/67531/metadc60515