Development of an Advanced Continuum Theory for Composite Laminates. Volume 2

Abstract

A continuum theory with a micro-macro structure was developed for composite laminates that satisfies the traction and displacement continuity requirements at interfaces. The interlaminar stresses were included in the model in a natural way and without any ad hoc assumptions. The built-in micro- structure of the continuum model can account for the effects of curvature and geometric nonlinearity. A set of constitutive relations in terms of material properties of individual constituents was developed which is capable of modeling fiber orientation and stacking sequence. The theory was further expanded to include the effects of temperature where a set of coupled thermo-mechanical field equations with corresponding constitutive relations were derived. Development of the theory for cylindrical and spherical geometries was completed and wave motions in flat and curved geometries was studied. A layerwise shear- deformable multi-director C(0) finite element formulation for the theory was developed which accounts for 3-D effects, allows thickness variation, and permits the warping of the deformed normal, while satisfying all continuity requirements.

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Document Details

Document Type
Technical Report
Publication Date
Dec 31, 1993
Accession Number
ADA277276

Entities

People

  • Arif Masud
  • G. R. Ghanimati
  • M. Panahandeh

Tags

Communities of Interest

  • Air Platforms
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Boundary Value Problems
  • Composite Materials
  • Differential Equations
  • Elastic Properties
  • Equations
  • Finite Element Analysis
  • Geometric Forms
  • Geometry
  • Laminates
  • Lines (Geometry)
  • Materials
  • Mechanics
  • Orientation (Direction)
  • Partial Differential Equations
  • Shape
  • Three Dimensional
  • Two Dimensional

Readers

  • Calculus or Mathematical Analysis
  • Structural Health Monitoring of Composite Structures.