Effects of Surface Roughness and Extreme Cooling on Boundary-Layer Transition for 15 Degrees Cone-Cylinder in Free Flight at Mach Numbers to 7.6 Metadata

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Title

  • Main Title Effects of Surface Roughness and Extreme Cooling on Boundary-Layer Transition for 15 Degrees Cone-Cylinder in Free Flight at Mach Numbers to 7.6
  • Series Title NACA Research Memorandums

Creator

  • Author: Rabb, Leonard
    Creator Type: Personal
  • Author: Krasnican, Milan J.
    Creator Type: Personal

Contributor

  • Originator: Lewis Flight Propulsion Laboratory
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab

Date

  • Creation: 1958-03-05

Language

  • English

Description

  • Content Description: Report presenting an investigation of three cone-cylinder bodies to obtain boundary-layer-transition data at very low ratios of wall to local stream temperature. Surface finishes at several levels of roughness height were tested. Results regarding the smooth body and rough bodies are provided.
  • Physical Description: 61 p. : ill.

Subject

  • Keyword: aerodynamics
  • Keyword: surface roughness

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: 78N78529
  • URL: http://hdl.handle.net/2060/19780078536
  • Report No.: NASA-TM-79867
  • Report No.: NACA-RM-E57K19
  • Center for AeroSpace Information Number: 19780078536
  • Archival Resource Key: ark:/67531/metadc53340
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