Comparison of experimental and theoretical normal-force distributions (including Reynolds number effects) on an ogive-cylinder body at Mach number 1.98 Metadata

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Title

  • Main Title Comparison of experimental and theoretical normal-force distributions (including Reynolds number effects) on an ogive-cylinder body at Mach number 1.98
  • Series Title NACA Research Memorandums

Creator

  • Author: Perkins, Edward W.
    Creator Type: Personal
  • Author: Jorgensen, Leland H.
    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: 1954-11-19

Language

  • English

Description

  • Content Description: Report presenting normal-force and pressure distributions for a body of revolution consisting of a fineness-ratio-3, circular-arc, ogival nose tangent to a cylindrical afterbody 7 diameters long. Comparisons of theoretical and experimental distributions indicate that available theoretical methods are only accurate for angles of attack up to about 5 degrees.
  • Physical Description: 50 p. : ill.

Subject

  • Keyword: pressure distributions
  • Keyword: aircraft design
  • Keyword: aerodynamics

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: 93R17783
  • URL: http://hdl.handle.net/2060/19930088493
  • Report No.: NACA-RM-A54H23
  • Center for AeroSpace Information Number: 19930088493
  • Archival Resource Key: ark:/67531/metadc60961
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