Evaluation of the C* Model for Addressing Short Fatigue Crack Growth

Abstract

The C* model has been proposed to account for the breakdown of K-similitude which occurs for short cracks. The model is based on the concept that crack growth rate is dependent not only on the stress intensity factor range, but also on crack length. This report evaluates the C* model using experimental data from the open literature. For comparison, two other models, the El Haddad model and the FASTRAN model, were also evaluated for their capability in dealing with the same problem. The objective of the evaluation was to assess the performance of the C* model compared with the other two models in treating short and long crack growth in a unified manner, and to illustrate their merits and shortcomings. For the cases tested, the C* model was found to be ineffective in resolving the issue of breakdown of similitude for short cracks, and was of less practical use than the other models.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 2008
Accession Number
ADA491888

Entities

People

  • K. F. Walker
  • Wenyi Hu

Organizations

  • Defence Science and Technology Group

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautics
  • Aircrafts
  • Airframes
  • Aluminum Alloys
  • Computer Programs
  • Damage Tolerance
  • Engineering
  • Experimental Data
  • Fatigue Life
  • Fracture (Mechanics)
  • Intensity
  • Materials
  • Mechanics
  • Military Aircraft
  • Stress Intensity Factors
  • Structural Integrity
  • Vehicles

Readers

  • Computational Modeling and Simulation
  • Materials Science (Mechanical Engineering).
  • Theoretical Analysis.