Studying the Effect of Residual Stresses on Fatigue Cracks Through Full-Field Methods (PREPRINT)

Abstract

In this effort, a corner crack was grown from a notch in a nickel-based superalloy specimen with a shot-peened surface treatment to induce residual stresses. The crack length was less than 200 microns, and the full displacement field near the crack was determined using advanced digital image correlation. The specimen was then annealed at elevated temperatures to reduce or eliminate the residual stresses, and the full displacement field near the crack was again determined. The displacements after annealing were indeed significantly larger than those previous to annealing, demonstrating the reduction in residual stresses. Modeling has been done to determine the approximate level of residual stresses induced and then reduced through annealing. Through this method, the effect of residual stresses on short fatigue cracks can be directly studied. Further work will be discussed on the effect of temperature on residual stresses, an area of great concern in predicting fatigue lives of components.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 2010
Accession Number
ADA523922

Entities

People

  • David A. Johnson
  • Dennis J. Buchanan
  • Reji John

Organizations

  • University of Dayton

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Air Force Research Laboratories
  • Applied Mechanics
  • Digital Cameras
  • Displacement
  • Images
  • Manufacturing
  • Materials
  • Mechanical Properties
  • Mechanics
  • Military Research
  • Residual Stress
  • Residuals
  • Shot Peening
  • Surface Finishing
  • United States

Readers

  • Semiconductor Device Technology
  • Structural Health Monitoring of Composite Structures.