STRESS WAVES IN COMPOSITE LAMINATES

Abstract

Fractures caused by stress waves resulting from hypervelocity impact are sometimes reduced, and at other times are increased, by the use of laminated materials. An analysis of some of the parameters which affect the ability of a laminated structure to resist fracture following impact has been conducted. It is shown that there are multiple reflections from the interfaces bounding any layer of material. The amplitudes of these waves attenuate very rapidly, but because their transmitted components may combine in phase with other waves, they sometimes contribute substantially to the total stress produced. It is shown that these combined waves may result in a stress much greater in the laminated material than would have been produced by the same impact on a solid target of either of the materials used; however, under other conditions, the laminate may be employed to reduce the stress to a very small value. Pressure pulse amplitudes in materials having impedance mismatch values ranging from 0.1 to 10. 0 and having as many as thirty laminations are presented in both graphical and tabular form.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1965
Accession Number
AD0465129

Entities

People

  • Ray Kinslow

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Composite Materials
  • Elastic Waves
  • Engineering
  • Explosives
  • Geometric Forms
  • Hypervelocity Impact
  • Laminates
  • Materials
  • Physical Properties
  • Pulse Amplitude
  • Secondary Waves
  • Shock Waves
  • Stress Waves
  • Stresses
  • Waves

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Structural Health Monitoring of Composite Structures.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers