On the Shear Strength of Skin-Stiffener Panels With Inspection Cut-Outs Metadata

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Title

  • Main Title On the Shear Strength of Skin-Stiffener Panels With Inspection Cut-Outs
  • Series Title NACA Wartime Reports
  • Series Title NACA Advanced Restricted Reports

Creator

  • Author: Kuhn, Paul
    Creator Type: Personal
  • Author: Diskin, Simon H.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1945-03

Language

  • English

Description

  • Content Description: "Strength tests and strain measurements were made of 19 long shear panels with rectangular inspection cut-outs; that is, cut-outs obtained by removing the sheet between two adjacent stringers without cutting any stringer. The test results indicated that the stress concentration existing at low stresses tends to disappear at very high stresses and that the assumption of uniform stress distribution leads to a satisfactory correlation of the test results. Stiffening of the sheet bay containing the cut-out was found to have practically no effect on the panel strength" (p. 1).
  • Physical Description: [16] p. : ill.

Subject

  • Keyword: material properties
  • Keyword: strength testing

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: 93R21827
  • URL: http://hdl.handle.net/2060/19930092537
  • Report No.: NACA-WR-L-192
  • Report No.: NACA-ARR-L5C01a
  • Center for AeroSpace Information Number: 19930092537
  • Archival Resource Key: ark:/67531/metadc60968
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