Supersonic flow past nonlifting bumped and indented bodies of revolution Metadata

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Title

  • Main Title Supersonic flow past nonlifting bumped and indented bodies of revolution
  • Series Title NACA Technical Notes

Creator

  • Author: McLean, F. Edward
    Creator Type: Personal
  • Author: Rennemann, Conrad, Jr.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1956-09

Language

  • English

Description

  • Content Description: Linear-theory values of the supersonic pressure field and wave drag of nonlifting bumped and indented bodies of revolution are presented and compared with the corresponding properties of a smooth body. The comparisons indicate that relatively small surface irregularities cause large pressure disturbances and changes in wave drag. The interference drag produced by bumps and indentations is discussed and a correction for the curvature of the characteristics is applied.
  • Physical Description: 40 p.

Subject

  • Keyword: aerodynamics
  • Keyword: irregular bodies of revolution

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: 93R13850
  • URL: http://hdl.handle.net/2060/19930084560
  • Report No.: NACA-TN-3744
  • Center for AeroSpace Information Number: 19930084560
  • Archival Resource Key: ark:/67531/metadc56069
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