Techniques for Flaw Detection in Composite Material Structures.

Abstract

This study concerns the nondestructive detection and quantification of flaws and voids in thin, cylindrical, fiber reinforced, composite, structures. Three types of flaws were investigated using shearing speckle and single beam speckle interferometry. The theory for each technique and photographs of the fringe patterns are presented. The Young's fringe method of speckle interferometry was used to determine the surface strains in the flaw region and the resulting flaw geometry was presented in graphical form. Shearing speckle interferometry was developed for a qualitative analysis only. The results show that flaws in their fiber reinforced composite structures can be detected and the size determined by either shearing speckle or single beam speckle interferometry. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1976
Accession Number
ADA036026

Entities

People

  • W. F. Ranson
  • W. F. Swinson

Organizations

  • Auburn University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Amplitude
  • Argon Lasers
  • Cameras
  • Cantilever Beams
  • Composite Materials
  • Composite Structures
  • Detection
  • Fiber Reinforced Composites
  • Geometry
  • Interferometry
  • Lasers
  • Light Sources
  • Materials
  • Photographs
  • Photography
  • Pressure Vessels
  • Spearography

Fields of Study

  • Physics

Readers

  • Optical Physics and Photonics.
  • Structural Health Monitoring of Composite Structures.