Off-Axis Impact of Unidirectional Composites with Cracks: Dynamic Stress Intensification.

Abstract

The dynamic response of unidirectional composites under off-axis (angle loading) impact is analyzed by assuming that the composite contains an initial flaw in the matrix material. The analytical method utilizes Fourier transform for the space variable and Laplace transform for the time variable. The off-axis impact is separated into two parts; one being symmetric and the other skew-symmetric with reference to the crack plane. Transient boundary conditions of normal and shear tractions are applied to a crack embedded in the matrix of the unidirectional composite. The two boundard conditions are solved independently and the results superimposed. Mathematically, these conditions reduce the problem to a system of dual integral equations which are solved in the Laplace transform plane for the transform of the dynamic stress intensity factor. The time inversion is carried out numerically for various combinations of the material properties of the composite and the results are displayed graphically. (AN)

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1979
Accession Number
ADA305097

Entities

People

  • E. P. Chen
  • George C. Sih

Organizations

  • Lehigh University

Tags

Communities of Interest

  • Air Platforms
  • C4I
  • Space

DTIC Thesaurus Topics

  • Aeronautics
  • Air Force
  • Aircrafts
  • Composite Materials
  • Crack Tips
  • Engineering
  • Failure Mode And Effect Analysis
  • Integral Equations
  • Jet Propulsion
  • Materials
  • Materials Laboratories
  • Mechanics
  • Navy
  • New Mexico
  • Physics Laboratories
  • Stress Waves
  • Stresses

Readers

  • Image Processing and Computer Vision.
  • Structural Dynamics.
  • Structural Health Monitoring of Composite Structures.

Technology Areas

  • Space
  • Space - Spacecraft Maneuvers