Modeling Localized Stress Fields in Composite Laminates.

Abstract

A structural model is developed using Reissner's variational principle to analyze stress gradient problems in laminated composite plates. A statically admissible stress field, which has explicit dependence on the thickness coordinate, is selected for each layer. Both interlaminar traction and displacement continuity are enforced between layers. This model is similar to an earlier one developed by Pagano, but has four dependent variables less per layer than Pagano's model. It is shown that the model can duplicate Pagano's results for the same number of subdivisions through the thickness. The uniform axial extension of a bidirectional symmetric laminate is used as the example problem for comparison to Pagano's theory and to illustrate the methodology. Originator-supplied keywords include: stress concentration, and Interlaminar stresses.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1984
Accession Number
ADA148630

Entities

People

  • E. R. Johnson

Organizations

  • Virginia Tech

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Composite Materials
  • Composite Structures
  • Delamination
  • Differential Equations
  • Engineering
  • Equations
  • Laminates
  • Materials
  • Materials Laboratories
  • Mathematical Models
  • Modulus Of Elasticity
  • Partial Differential Equations
  • Physics Laboratories
  • United States
  • Universities
  • Virginia

Readers

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