An Investigation of Stress Corrosion Crack Arrest and Crack Propagation in a Titanium Alloy

Abstract

It was previously demonstrated that the controlling crack growth criterion in stress corrosion cracking is that derived from fracture mechanics concepts and not a criterion based on gross or net stress. This demonstration was accomplished by testing two types of cracked specimens and showing that crack arrest and crack initiation stress intensities are the same while gross and net stresses are different. However, these tests were performed on thick section material. The work now reported was intended to check the validity of the correlation between arrest and initiation stress intensities using thin section material having higher thoughness and lower yield strength than the material previously tested. The results showed crack arrest stress intensities were substantially higher than those for crack initiation when testing thin materials. It was also observed from the test results that when testing titanium materials testing must be accomplished as soon as possible after fatigue cracking to eliminate any possible effects of crack blunting.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1970
Accession Number
AD0720235

Entities

People

  • Gerald J. Petrak

Organizations

  • University of Dayton

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Alkanes
  • Corrosion
  • Crack Propagation
  • Crack Tips
  • Cracks
  • Fatigue Cracking
  • Fracture (Mechanics)
  • Government Procurement
  • Materials
  • Materials Laboratories
  • Materials Testing
  • Mechanics
  • Stress Corrosion
  • Stress Corrosion Cracking
  • Stress Intensity Factors
  • Titanium

Fields of Study

  • Engineering

Readers

  • Cardiovascular Physiology
  • Reinforced Composite Materials
  • Systems Analysis and Design