Transonic Flow Past Cone Cylinders Metadata

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Title

  • Main Title Transonic Flow Past Cone Cylinders
  • Series Title NACA Technical Notes

Creator

  • Author: Solomon, George E.
    Creator Type: Personal

Contributor

  • Originator: United States. National Advisory Committee for Aeronautics.
    Contributor Type: Organization

Date

  • Creation: 1954-09

Language

  • English

Description

  • Content Description: Note presenting experimental results for transonic flow past cone-cylinder, axially symmetric bodies. The drag coefficient and surface Mach number are studied as the free-stream Mach number is varied and, wherever possible, the experimental results are compared with theoretical predictions. The theoretical problem of transonic flow past finite cones is discussed briefly and an approximate solution of the axially symmetric transonic equations, valid for a semi-infinite cone, is presented.
  • Physical Description: 56 p. : ill.

Subject

  • Keyword: flow characteristics
  • Keyword: transonic flow
  • Keyword: cone cylinders

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: 93R13363
  • URL: http://hdl.handle.net/2060/19930084073
  • Report No.: NACA-TN-3213
  • Center for AeroSpace Information Number: 19930084073
  • Archival Resource Key: ark:/67531/metadc57352
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