Compressive Buckling of Flat Rectangular Metalite Type Sandwich Plates With Simply Supported Loaded Edges and Clamped Unloaded Edges

Abstract

A theoretical solution is obtained for the problem of the compressive buckling of flat rectangular Metalite type sandwich plates with simply supported loaded edges and clamped unloaded edges. The solution is based upon the general small-deflection theory for flat sandwich plates developed in NACA TN No l526. Good agreement is found between the present results and those of Forest Products Laboratory Rep. No. l583. A comparison of computed arid experimental buckling stresses of sandwich plates with balsa-wood cores and with cellular-cellulose-acetate cores indicates reasonable agreement between theoretical and experimental results.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1949
Accession Number
ADA380573

Entities

People

  • Paul Seide

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Acetates
  • Aeronautical Laboratories
  • Agreements
  • Air Force
  • Air Force Facilities
  • Aluminum Alloys
  • Aspect Ratio
  • Bending Moments
  • Boundaries
  • Cellulose Acetates
  • Differential Equations
  • Equations
  • Materials
  • Modulus Of Elasticity
  • Plastic Properties
  • Shear Modulus
  • Stiffness

Fields of Study

  • Physics

Readers

  • Structural Dynamics.