Experimental Measurements of Forces and Moments on a Two-Dimensional Oscillating Wing at Subsonic Speeds Metadata

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Title

  • Main Title Experimental Measurements of Forces and Moments on a Two-Dimensional Oscillating Wing at Subsonic Speeds
  • Series Title NACA Technical Notes

Creator

  • Author: Clevenson, Sherman A.
    Creator Type: Personal
  • Author: Widmayer, Edward, Jr.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1956-06

Language

  • English

Description

  • Content Description: "Experimental results of lifts and moments about the quarter chord of a two-dimensional wing at subsonic Mach numbers are presented. A comparison of the experimental magnitude of the lift vector with the theory as given by Dietze showed good agreement. Comparisons of the moments and the quadrature component of lift with theory indicated that some refinements in the testing technique are necessary for the experimental determination of these quantities in the transonic range" (p. 1).
  • Physical Description: 28 p. : ill.

Subject

  • Keyword: aerodynamics
  • Keyword: aircraft stability
  • Keyword: oscillating lifts

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: 93R13710
  • URL: http://hdl.handle.net/2060/19930084420
  • Report No.: NACA-TN-3686
  • Center for AeroSpace Information Number: 19930084420
  • Archival Resource Key: ark:/67531/metadc55939
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