Buckling of Eccentrically Stiffened Orthotropic Cylinders Under Pure Bending.

Abstract

The stability of stiffened orthotropic cylinders which include the effects of eccentric stiffeners and are loaded with pure bending or any combination of bending and compression is investigated analytically by means of a small deflection theory. Solutions to the buckling equations are obtained for simple support boundary conditions by use of the Galerkin method. The pure bending buckling loads are compared with existing pure compression buckling loads for three contemporary cylinder configurations. Also shown are predicted buckling modes and typical interaction curves between bending and compression. The results show that eccentricity effects are substantial and that the maximum pure bending load may be as much as 40 percent greater than the pure compression load.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1966
Accession Number
ADA307274

Entities

People

  • David L. Block

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aeronautics
  • Boundaries
  • Buckling
  • Coefficients
  • Compression
  • Eccentricity
  • Elastic Properties
  • Equations
  • Foreign Languages
  • Galerkin Method
  • Materials
  • Modulus Of Elasticity
  • Shape
  • Shear Modulus
  • Stiffened Cylinders
  • Stiffening
  • Stiffness

Readers

  • Structural Dynamics.