Time - Domain First Born Approximations to Elastodynamic Backscatter with Applications to Non-Destructive Evaluation of Composites.

Abstract

Fiber-reinforced composite materials are bieng introduced into primary structures of modern jet fighter aircraft, e.g., vertical and horizontal stabilizers on the F-15 and F-16 fighters. These materials are made of many layers; each layer consists of many rows of parallel fibers bound together by a matrix material of different composition than the fibers. Failure often occurs in these composites via delamination which initiates at gas bubbles (porosity) remaining in the matrix after the manufacturing process. For this and other reasons, non-destructive inspection techniques capable of determining the presence of the porosity are being sought. Current efforts include inspection with elastic waves. Items of interest include comparison of the response from the fibers to that from porosity and the degree to which the fibers may appear transparent to the waves.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1982
Accession Number
ADA123541

Entities

People

  • Gregory T. Warhola

Organizations

  • Wright Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Born Approximations
  • Composite Materials
  • Elastic Materials
  • Elastic Waves
  • Fiber Reinforced Composites
  • Frequency
  • Inspection
  • Long Wavelengths
  • Materials
  • Materials Laboratories
  • Plane Waves
  • Porosity
  • Scattering
  • Stiffness
  • Waveforms
  • Waves

Fields of Study

  • Materials science

Readers

  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Reinforced Composite Materials
  • Structural Health Monitoring of Composite Structures.