Compression Test Simulation of Thick-Section Composite Materials

Abstract

An improved compression test concept for thick-section composite materials based on a stress analysis simulation study is presented. An end loading method involving specimen support by a locked hemispherical seat was identified as the most desirable. The results showed that this method could substantially reduce the stress variation due to specimen imperfection and loading eccentricity. Compression test methods are analyzed using a finite element methodology. Limitations of the test methods are identified with respect to their ability to obtain the desired uniform stress field. The end loading method proved to be superior to the side loading method for the thick-section composite material. The frictional forces introduced by the end loading method can reduce local failure at the specimen end. The zone of end effects on the stress distribution was obtained for the composite material.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1992
Accession Number
ADA255021

Entities

People

  • Tzi-kang Chen

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Composite Materials
  • Eccentricity
  • Engineering
  • Failure Mode And Effect Analysis
  • Materials
  • Materials Science
  • Materials Testing
  • Mechanical Properties
  • Mechanics
  • Military Research
  • Modulus Of Elasticity
  • Simulations
  • Stresses
  • Test And Evaluation
  • Test Methods

Fields of Study

  • Engineering

Readers

  • Structural Dynamics.
  • Structural Health Monitoring of Composite Structures.