Accession Number : ADA132162

Title :   Evaluation of Stress Corrosion Cracking Characteristics of Selected Fastener Systems in 7075-T6 Aluminum.

Descriptive Note : Final rept. Nov 81-Nov 82,

Corporate Author : AIR FORCE WRIGHT AERONAUTICAL LABS WRIGHT-PATTERSON AFB OH

Personal Author(s) : Ontko,Neal R

PDF Url : ADA132162

Report Date : Jun 1983

Pagination or Media Count : 40

Abstract : This effort evaluated the stress corrosion cracking characteristics of selected fatigue rated fastener systems in 7075-T6 Aluminum extruded material. The fastener systems used were installed with equivalent amounts of interference in the test blocks and subjected to 1700 hours of alternate immersion exposure in 3.5 % salt water. (Author)

Descriptors :   *Aluminum, Aluminum alloys, Fastenings, Stress corrosion, Cracking(Fracturing), Test and evaluation, Fatigue(Mechanics), Salt water, Cold working, Expansion, Steel, Cadmium

Subject Categories : Properties of Metals and Alloys
      Couplers, Fasteners, and Joints
      Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE