The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow Metadata

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Title

  • Main Title The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow
  • Series Title NACA Research Memorandums

Creator

  • Author: Love, Eugene S.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1952-11-12

Language

  • English

Description

  • Content Description: Report presenting the results of an investigation to determine the effects of a small jet of air exhausting from the nose of an elliptical body of revolution upon boundary-layer transition and the viscous, pressure, and total drag of the forebody at three body stations at Mach number 1.62. The jet effects on body pressure, pressure variations, boundary-layer transition, and total drag are provided.

Subject

  • Keyword: aerodynamics
  • Keyword: body pressure

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: 93R16648
  • URL: http://hdl.handle.net/2060/19930087358
  • Report No.: NACA-RM-L52I19a
  • Center for AeroSpace Information Number: 19930087358
  • Archival Resource Key: ark:/67531/metadc279634