Critical Compressive Stress for Outstanding Flanges Metadata

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  • Main Title Critical Compressive Stress for Outstanding Flanges
  • Series Title NACA Technical Reports


  • Author: Lundquist, Eugene E.
    Creator Type: Personal
  • Author: Stowell, Elbridge Z.
    Creator Type: Personal


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


  • Creation: 1941-03-14


  • English


  • Content Description: A chart is presented for the values of the coefficient in the formula for the critical compressive stress at which buckling may be expected to occur in outstanding flanges. These flanges are flat rectangular plates supported along the loaded edges, supported and elastically restrained along one unloaded edge, and free along the other unloaded edge. The mathematical derivations of the formulas required for construction of the chart are given.
  • Physical Description: 111 - 121 p. : ill.


  • Keyword: compressive stress
  • Keyword: outstanding flanges


  • Name: National Advisory Committee for Aeronautics Collection
    Code: NACA
  • Name: Technical Report Archive and Image Library
    Code: TRAIL


  • Name: UNT Libraries Government Documents Department
    Code: UNTGD


  • Rights Access: public
  • Rights License: pd
  • Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available

Resource Type

  • Report


  • Text


  • Accession or Local Control No: 93R21102
  • URL:
  • Report No.: NACA-TR-734
  • Center for AeroSpace Information Number: 19930091812
  • Report No.: NACA-SR-188
  • Archival Resource Key: ark:/67531/metadc59989