Aeronautical Analytical Rework Program: Acoustical Holography System Demonstration on A-6 Wing Skin Stiffener Acoustic Image Inspection.

Abstract

The objective of the work reported in this document was to demonstrate the applicability of acoustical imaging techniques using the System 200 Acoustical Holography Inspection System to inspect naval aircraft, in particular the A-6 wing skin stiffener. The successful results obtained in this applicability test reflect the capability of the System 200 Acoustical Holography Inspection System to provide repeatable hard-copy evidence of the integrity of structures such as the A-6 wing skin stiffener.

Document Details

Document Type
Technical Report
Publication Date
May 28, 1975
Accession Number
ADA012584

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Acoustic Images
  • Aircrafts
  • Demonstrations
  • Hard Copy
  • Holography
  • Images
  • Imaging Techniques
  • Inspection
  • Mechanical Structure

Fields of Study

  • Physics

Readers

  • Facility/Structural Engineering.
  • Optical Physics and Photonics.
  • Structural Dynamics.