Buckling of Unidirectional Graphite/Epoxy Composite Plates at Low Temperatures

Abstract

A theoretical and experimental study of the buckling and postbuckling behavior of unidirectionally laminated graphite/epoxy plates was conducted under combined thermal cooling and compressive loading. The rectangular plates were simply supported at the loaded edges and free in the remaining edges. The plates were found to bend during cooling even without mechanical loads because of the negative thermal expansion coefficient of the material in the loading direction and the in-plane end constraints at the two-loaded edges. Such bending from thermal load was treated as an initial geometric imperfection, and the analysis was based on Koiter's theory of elastic stability. The experimental postbuckling curves agreed well with the theoretical values.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1991
Accession Number
ADA246602

Entities

People

  • David Hui
  • Piyush K. Dutta
  • Yvonne M. Traynham

Organizations

  • Cold Regions Research and Engineering Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Buckling
  • Coefficients
  • Cold Regions
  • Composite Materials
  • Engineering
  • Epoxy Composites
  • Epoxy Laminates
  • Graphitic Materials
  • Laminates
  • Low Temperature
  • Materials
  • Materials Laboratories
  • Mechanics
  • New York
  • Reinforced Plastics
  • Strain Gages
  • Thermal Expansion

Fields of Study

  • Physics

Readers

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