Two-dimensional chord-wise load distributions at transonic speeds Metadata

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Title

  • Main Title Two-dimensional chord-wise load distributions at transonic speeds
  • Series Title NACA Research Memorandums

Creator

  • Author: Lindsey, Walter F.
    Creator Type: Personal
  • Author: Dick, Richard S.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1952-02-18

Language

  • English

Description

  • Content Description: Report presenting testing on the NACA 16-009 airfoil and on eight airfoils of the NACA 6A series, which shows that the chordwise loading due to lift at a Mach number of 1.0 is insignificantly affected by thickness distribution within the range of airfoil shapes presented and only slightly affected by thickness. Results regarding the experimental loading on symmetrical airfoils, method of estimating pressure distribution, experimental loadings on cambered airfoils, and scope of method are provided.
  • Physical Description: 41 p. : ill.

Subject

  • Keyword: airfoils
  • Keyword: aircraft loading

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: 93R16086
  • URL: http://hdl.handle.net/2060/19930086796
  • Report No.: NACA-RM-L51I07
  • Center for AeroSpace Information Number: 19930086796
  • Archival Resource Key: ark:/67531/metadc58975