PERTURBATION SOLUTIONS FOR THE BUCKLING PROBLEM OF AXIALLY COMPRESSED THIN CYLINDER SHELLS

Abstract

A study is made of the effect of initial deviations on the load carrying capacity of thin circular cylindrical shells under uniform axial compression. A perturbation expansion is used to reduce the nonlinear equations of von Karman-Donnell to an infinite set of linear equations, of which only the first few need be solved to obtain a reasonable accurate solution. The results for both infinite shells and shells of finite length indicate that a small imperfection can sharply reduce the maximum load that a thin-walled cylinder will sustain. In addition, for a particular set of boundary conditions, it is shown that the effect of the length for a finite shell, is small.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1966
Accession Number
AD0642939

Entities

People

  • Clive L. Dym
  • Nicholas J. Hoff

Organizations

  • Stanford University

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aeronautics
  • Air Force
  • Astronautics
  • Computational Science
  • Differential Equations
  • Digital Computers
  • Equations
  • Fluid Mechanics
  • Mechanics
  • Modulus Of Elasticity
  • Nonlinear Differential Equations
  • Partial Differential Equations
  • Payload
  • Perturbations
  • Potential Energy
  • Power Series
  • Shape

Fields of Study

  • Engineering
  • Physics

Readers

  • Structural Dynamics.