Frequency and Mean Stress Effects in High Cycle Fatigue of Ti-6Al-4V

Abstract

The objective of this project was to extend past research on fatigue of Ti-6Al-4V into conditions which more closely reflect actual use conditions. This included testing at a range of frequencies (70, 400, 1800 Hz) to determine the effect of frequency on the fatigue strength. In addition, testing was performed at various stress ratios (0.1, 0.5, 0.8) to determine the effects of mean stress on the HCF performance of Ti-6A1-4V. This included an examination of the effects of cyclic and time-dependent strain accumulation on the fracture mode at high mean stresses. Frequency effects were observed at low stress ratios, resulting in higher fatigue strengths as the frequency increased. Possible causes include strain rate effects on dislocation motion, loss of active primary slip systems at high frequencies in hexagonal close-packed and body-centered cubic materials, and environmental damage. Results obtained at high mean stress show that the behavior of Ti-6A1-4V consists of a complex combination of fatigue, cyclic creep, and strain ratchetting. Fractographic analysis combined with cyclic creep studies were used to further define the mechanisms which led to the observed behavior.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1997
Accession Number
ADA330696

Entities

People

  • Ryan Morrissey

Tags

Communities of Interest

  • Air Platforms
  • C4I

DTIC Thesaurus Topics

  • Air Force
  • Corrosion Resistance
  • Crack Propagation
  • Creep Tests
  • Crystal Structure
  • Dislocations
  • Failure Mode And Effect Analysis
  • Fatigue Tests (Mechanics)
  • Frequency
  • Gas Turbines
  • Load Cells
  • Materials
  • Measurement
  • Mechanics
  • Strain Rate
  • Titanium Alloys
  • Turbines

Readers

  • Mechanical Engineering/Mechanics of Materials.
  • Powder metallurgy of Titanium alloys.
  • Structural Health Monitoring of Composite Structures.