Laser Shock Peened Compressive Residual Profile after Exposure to Temperature.

Abstract

The surface of any component that undergoes mechanical loading is particularly important in influencing the fatigue life of that part. The factors that contribute to surface fatigue sensitivity are less slip restriction at the surface, the existence of single edge cracks, the surface sees large tensile gradients when the part is exposed to bending and torsion, the surface tends to be an area of multiple defects and the surface is the most sensitive region to environmental effects such as corrosion. Compressive residual stresses are utilized in the turbine engine environment to counteract regions on the surface that must withstand high tensile stresses.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1995
Accession Number
ADA305914

Entities

People

  • Chris Lykins
  • Paul Prevey
  • Perry Mason

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Cold Working
  • Corrosion
  • Diffraction
  • Environment
  • Hydrogen Embrittlement
  • Manufacturing
  • Materials
  • Residual Stress
  • Residuals
  • Sensitivity
  • Shot Peening
  • Stress Corrosion
  • Stresses
  • Tensile Stress
  • Turbines
  • X Rays

Readers

  • Fluid Dynamics.
  • Structural Health Monitoring of Composite Structures.

Technology Areas

  • Directed Energy