Compressive Buckling of Simply Supported Plates With Longitudinal Stiffeners Metadata

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Title

  • Main Title Compressive Buckling of Simply Supported Plates With Longitudinal Stiffeners
  • Series Title NACA Technical Notes

Creator

  • Author: Seide, Paul
    Creator Type: Personal
  • Author: Stein, Manuel
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1949-03

Language

  • English

Description

  • Content Description: "Charts are presented for the analysis of the stability under compression of simply supported rectangular plates with one, two, three, and an infinite number of identical equally spaced longitudinal stiffeners that have zero torsional stiffness" (p. 1).
  • Physical Description: 23 p. : ill.

Subject

  • Keyword: rectangular plates
  • Keyword: longitudinal stiffeners
  • Keyword: stability analysis

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: 93R11800
  • URL: http://hdl.handle.net/2060/19930082510
  • Report No.: NACA-TN-1825
  • Center for AeroSpace Information Number: 19930082510
  • Archival Resource Key: ark:/67531/metadc55144