Mechanisms of Corrosion Fatigue of Aluminum Alloys.

Abstract

An overview of experimental variables which are considered critical to understanding the mechanisms of corrosion fatigue of high strength aluminum alloys is presented. Based on this overview, an examination of previously proposed mechanisms is attempted. These models include anodic dissolution, surface energy reduction, and hydrogen embrittlement. It is concluded that hydrogen embrittlement of process zones at alloy surfaces (for crack initiation) and at crack tips (for crack propagation) best explains observed results. A general model of corrosion fatigue of these alloys is proposed. This model suggests that the nature of the naturally formed oxide film on aluminum alloys may be a critical factor. Chemical or mechanical damage of the film allows hydrogen ingress. The presence of second phase particles which may act as sinks for dislocation transported hydrogen, may also be a necessary prerequisite to significant amounts of reduction in fatigue resistance associated with corrosion. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1981
Accession Number
ADA097912

Entities

People

  • David J. Duquette

Organizations

  • Rensselaer Polytechnic Institute

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aluminum Alloys
  • Chemistry
  • Corrosion
  • Crack Propagation
  • Crack Tips
  • Cracks
  • Heat Treatment
  • Hydrogen Embrittlement
  • Materials
  • Materials Engineering
  • Mechanical Properties
  • Mechanics
  • Oxide Films
  • Stress Corrosion
  • Stress Corrosion Cracking
  • Surface Energy
  • Water Vapor

Fields of Study

  • Materials science

Readers

  • Materials Science and Engineering.
  • Structural Health Monitoring of Composite Structures.
  • Surface Engineering/Surface Coating Technology.

Technology Areas

  • AI & ML