Torsion Tests of Stiffened Circular Cylinders Metadata

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Title

  • Main Title Torsion Tests of Stiffened Circular Cylinders
  • Series Title NACA Wartime Reports
  • Series Title NACA Advanced Restricted Reports

Creator

  • Author: Moore, R. L.
    Creator Type: Personal
  • Author: Wescoat, C.
    Creator Type: Personal

Contributor

  • Originator: Aluminum Company of America
    Contributor Type: Organization

Date

  • Creation: 1944-05

Language

  • English

Description

  • Content Description: "The design of curved sheet panels to resist shear involves a consideration of several factors: the buckling resistance of the sheet, the stress at which buckling becomes permanent, and the strength which may be developed beyond the buckling limit by tension-field action. Although some experimental as well as theoretical work has been done on the buckling and tension-field phases of this problem, neither of these types of action appears to be very well understood. This report presents the results of the first series of torsion tests of stiffened circular cylinders to be completed in connection with this study at Aluminum Research Laboratories" (p. 1).
  • Physical Description: [56] p. : ill.

Subject

  • Keyword: aircraft design
  • Keyword: metallic properties
  • Keyword: curved sheet panels

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: 93R20219
  • URL: http://hdl.handle.net/2060/19930090929
  • Report No.: NACA-WR-W-89
  • Report No.: NACA-ARR-4E31
  • Center for AeroSpace Information Number: 19930090929
  • Archival Resource Key: ark:/67531/metadc65450
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