On the Analysis of Anisotropic Rectangular Plates

Abstract

Extensive use of energy methods in conjunction with classical beam mode functions has been used to obtain approximate solutions to homogeneous, or symmetrically laminated, anisotropic plate problems. Because of the existence of cross- elasticity bending stiffness terms, the beam functions do not satisfy the natural boundary conditions. As a result, bending moments and stresses, which are of practical interest, may converge to the wrong solution or may not converge at all. Furthermore, bending deflections, buckling loads, and fundamental vibration frequencies converge very slowly for highly anisotropic materials. This report shows that improved results can be obtained for anisotropic plates which contain strong cross-elasticity effects by using a classical Fourier analysis which satisfies both the geometric and natural boundary conditions. Numerical results are presented for bending under transverse load, buckling under biaxial compression and pure shear, and natural frequencies of flexural vibrations. Both homogeneous and laminated plates are discussed.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1972
Accession Number
AD0776017

Entities

People

  • J. M. Whitney

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Bending Moments
  • Boundaries
  • Buckling
  • Composite Materials
  • Deflection
  • Elastic Properties
  • Epoxy Composites
  • Fourier Analysis
  • Fourier Series
  • Frequency
  • Laminates
  • Materials
  • Materials Laboratories
  • Orientation (Direction)
  • Stiffness
  • Vibration

Readers

  • Approximation Theory.
  • Mechanical Engineering/Mechanics of Materials.
  • Plasma Physics / Magnetohydrodynamics