Free-flight tests of 45 degree swept wings of aspect ratio 3.15 and taper ratio 0.54 to measure wing damping of the first bending mode and to investigate the possibility of flutter at transonic speeds Metadata

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Title

  • Main Title Free-flight tests of 45 degree swept wings of aspect ratio 3.15 and taper ratio 0.54 to measure wing damping of the first bending mode and to investigate the possibility of flutter at transonic speeds
  • Series Title NACA Research Memorandums

Creator

  • Author: O'Kelly, Burke R.
    Creator Type: Personal
  • Author: Lundstrom, Reginald R.
    Creator Type: Personal
  • Author: Lauten, William T., Jr.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1954-10-12

Language

  • English

Description

  • Content Description: Report presenting free-flight tests made on two pairs of wings of aspect ratio 3.15, taper ratio 0.54, and 45 degrees sweepback in the transonic speed range to measure wing damping and to investigate the possibility of flutter. Results regarding the flight test and analysis and discussion are provided.
  • Physical Description: 24 p. : ill.

Subject

  • Keyword: aircraft wings
  • Keyword: wing damping

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: 93R17494
  • URL: http://hdl.handle.net/2060/19930088204
  • Report No.: NACA-RM-L54C22
  • Center for AeroSpace Information Number: 19930088204
  • Archival Resource Key: ark:/67531/metadc60398