Effects of Boundary-Layer Separation on Normal Force and Center of Pressure of a Cone-Cylinder Model With a Large Base Flare at Mach Numbers From 3.00 to 6.28 Metadata

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Title

  • Main Title Effects of Boundary-Layer Separation on Normal Force and Center of Pressure of a Cone-Cylinder Model With a Large Base Flare at Mach Numbers From 3.00 to 6.28
  • Series Title NACA Research Memorandums

Creator

  • Author: Dennis, David H.
    Creator Type: Personal
  • Author: Syvertson, Clarence A.
    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: 1955-10-03

Language

  • English

Description

  • Content Description: Report presenting testing of a body with a 22.5 degree conical nose, a 4-diameter-long cylindrical midsection, and a 20 degree cone-frustum tail flare. The tests were made over a variety of angles of attack and Mach numbers. Results regarding spark shadowgraph pictures and predictions versus the actual values were provided.
  • Physical Description: 14 p. : ill.

Subject

  • Keyword: aircraft design
  • Keyword: flow separation

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: 93R18305
  • URL: http://hdl.handle.net/2060/19930089015
  • Report No.: NACA-RM-A55H09
  • Center for AeroSpace Information Number: 19930089015
  • Archival Resource Key: ark:/67531/metadc61947
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