Microstructurally Based Model of Fatigue Initiation and Growth

Abstract

A model to calculate fatigue life is developed based on the assumption that fatigue life is entirely composed of crack growth from an initial microstructural inhomogeneity. Specifically, growth is considered to start from either an ellipsoidal void, a cracked particle, or a debonded particle. The capability for predicting fatigue life from material microstructure is based on linear elastic fracture mechanics principles, the sizes of the crack-initiating microstructural inhomogeneities, and an initiation parameter that is proportional to the cyclic plastic zone size. A key aspect of this modeling approach is that it is linked with a general purpose probability program to analyze the effect of the distribution of controlling microstructural features within the material. This enables prediction of fatigue stress versus life curves for various specimen geometries using distributional statistics obtained from characterizations of the microstructure. Results are compared to experimental fatigue data from an aluminum alloy.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Apr 07, 1994
Accession Number
ADA278198

Entities

People

  • A. J. Hinkle
  • J. R. Brockenbrough
  • P. E. Magnusen
  • R. J. Bucci

Organizations

  • Alcoa

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Alloys
  • Aluminum Alloys
  • Aspect Ratio
  • Electron Microscopes
  • Failure Mode And Effect Analysis
  • Far Field
  • Fatigue Life
  • Fatigue Tests (Mechanics)
  • Fracture (Mechanics)
  • Materials
  • Mechanics
  • Particle Size
  • Sensitivity
  • Shape
  • Stress Concentration
  • Stress Intensity Factors
  • Yield Strength

Fields of Study

  • Materials science

Readers

  • Calculus or Mathematical Analysis
  • Computational Modeling and Simulation
  • Materials Science (Mechanical Engineering).