Experimental and Theoretical Assessment of a New Technique for the Non-Destructive Evaluation of Laminated Panels.

Abstract

The goal of the present research project was to evaluate a potential method of edge flaw detection in laminated structures. This method uses miniature dynamic force transducers to detect the changes in loading history arising from the (very low level) impact of steel spheres on the transducer, which is located on the surface of the examined object. A theoretical and experimental analysis of the low frequency vibration response of bonded joints showed that it is possible to distinguish between mechanically sound and debonded specimen using a low frequency analysis. This analysis has shown that it is possible to construct a field-usable instrument that would permit rapid inspection of bonded structures for degrading conditions that occur at the edges of bonded joints. This analysis is applicable to both composite and metal laminated structures. Keywords: Adhesive bond quality control; Laminated panel quality control; Plate waves; Finite element modeling; Laminates; Laminated composite materials.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Feb 21, 1985
Accession Number
ADA155622

Entities

People

  • V. H. Kenner

Organizations

  • Ohio State University

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • C4I
  • Sensors

DTIC Thesaurus Topics

  • Bonded Joints
  • Composite Materials
  • Epoxy Composites
  • Finite Element Analysis
  • Frequency
  • Inspection
  • Joints
  • Materials
  • Materials Laboratories
  • Materials Processing
  • Measurement
  • Mechanics
  • Resonant Frequency
  • Test And Evaluation
  • Two Dimensional
  • Vibration
  • Waves

Readers

  • Aerospace Test and Evaluation
  • Structural Health Monitoring of Composite Structures.