Accession Number:

ADA012584

Title:

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

Descriptive Note:

Interim rept.

Corporate Author:

HOLOSONICS INC RICHLAND WASH

Personal Author(s):

Report Date:

1975-05-28

Pagination or Media Count:

27.0

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.

Subject Categories:

  • Attack and Fighter Aircraft
  • Test Facilities, Equipment and Methods

Distribution Statement:

APPROVED FOR PUBLIC RELEASE