Finite-Element Analysis of Laminated Composite-Material Plates.

Abstract

A finite-element formulation of the equations governing the laminated anisotropic plate theory of Yang, Norris and Stavsky, is presented. The theory is a generalization of Mindlin's theory for isotropic plates to laminated anisotropic plates and includes shear deformation and rotary inertia effects. Finite-element solutions are presented for rectangular plates of antisymmetric angle-ply laminates having material properties that are typical of a highly anisotropic composite material. Two sets of material properties that are typical of advanced fiber-reinforced composites are used to show the parametric effects of plate aspect ratio, length-to-thickness ratio, number of layers, and lamination angle. The element is also employed to study the bending of laminated, anisotropic bimodulus material-plates. Results are presented for single-layer and two-layer cross-ply rectangular plates subjected to sinusoidal loading. The report also presents a C deg. finite element for the von Karman equations of thin elastic plates.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1979
Accession Number
ADA071390

Entities

People

  • Junuthula N. Reddy

Organizations

  • University of Oklahoma

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Accuracy
  • Aspect Ratio
  • Composite Materials
  • Elastic Properties
  • Energy
  • Equations
  • Equations Of Motion
  • Fiber Reinforced Composites
  • Finite Element Analysis
  • Frequency
  • Laminates
  • Materials
  • Mechanics
  • Potential Energy
  • Thickness
  • Transverse
  • Vibration

Readers

  • Structural Dynamics.