STRESS CORROSION CRACKING IN AIRCRAFT STRUCTURAL MATERIALS

Abstract

Contents: General theory of stress corrosion; Laboratory aspects of aluminium alloys; Some engineering aspects of stress corrosion cracking in high strength aluminium alloys; Engineering aspects of stress corrosion failure in martensitic steels; Stress corrosion cracking of high strength stainless steels; Stress corrosion of titanium alloys; Stress corrosion cracking of very strong low alloy and maraging steels: laboratory aspects; National surveys of work on stress corrosion cracking.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1967
Accession Number
AD0669282

Entities

Organizations

  • AGARD

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Energy and Power Technologies
  • Engineered Resilient Systems
  • Ground and Sea Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Chemical Synthesis
  • Chemistry
  • Manufacturing
  • Materials
  • Materials Engineering
  • Materials Science
  • Materials Testing
  • Mechanical Working
  • Mechanics
  • Rocket Oxidizers
  • Sheet Metal
  • Solid Solutions

Fields of Study

  • Materials science

Readers

  • Materials Science (Mechanical Engineering).