Accession Number:

ADA149234

Title:

Tensile and Fracture Toughness Properties of Mirage III Spars.

Descriptive Note:

Technical memo.,

Corporate Author:

AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA)

Personal Author(s):

Report Date:

1984-04-01

Pagination or Media Count:

17.0

Abstract:

Tensile and fracture toughness tests were conducted on specimens manufactured from the flange portions of the main spars of seven Mirage III wings. These have provided specific information relating to the mechanical properties of this component at locations close to where fatigue cracking occurred in service. Author.

Subject Categories:

  • Aircraft
  • Metallurgy and Metallography
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE