Influence of Yield Strength on Overload Affected Fatigue Crack Growth Behavior in 4340 Steel

Abstract

Single tensile overloads were applied to 4340 steel specimens which were treated to give 120 and 220 ksi yield strength levels. The influence of yield strength level on the number of nonsteady state crack growth cycles subsequent to the application of a 100 percent overload was noted to be substantial. The number of nonsteady state cycles for the 120 ksi strength steel was approximately an order of magnitude greater than that of the higher strength steel. A retardation model was developed using a residual stress intensity factor concept similar to that proposed by Willenborg et al. The model was found to predict to within 10 percent the number of nonsteady state crack growth cycles required to move a crack from the pre-overload position to a subsequent position, one overload induced plane stress plastic zone radius ahead of the pre-overload position. The model indicates that the reason for substantial increase in nonsteady state crack growth cycles observed for the low strength steel is due to a corresponding increase in the overload affected zone size.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1974
Accession Number
AD0787655

Entities

People

  • J. P. Gallagher
  • T. F. Hughes

Organizations

  • Flight Dynamics Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Crack Propagation
  • Equations
  • Fracture (Mechanics)
  • Geometry
  • Intensity
  • Materials
  • Mechanics
  • Residual Stress
  • Residuals
  • Retardation
  • Steady State
  • Stress Intensity Factors
  • Stresses
  • Test Methods
  • Yield Strength

Fields of Study

  • Materials science

Readers

  • Combustion science or combustion engineering.
  • Materials Science (Mechanical Engineering).