Load Ratio Dependence of Fatigue Threshold in Aermet 100 Steel,

Abstract

A study was conducted on the fatigue crack growth behavior of AerMet 100 steel at various load ratios in a gaseous dry nitrogen environment. Increasing the load ratio increased the near-threshold fatigue crack growth rate and reduced the threshold stress intensity range for fatigue crack growth, DeltaK sub th. DeltaK sub th decreased with increasing load ratio up to a critical value, R sub cr = 0.5, and then leveled off. The maximum stress intensity at threshold, K sub max, changed little below R sub cr but increased rapidly above R sub cr. The critical threshold stress intensity range, DeltaK sub th and the critical maximum stress intensity, K max were determined to be 2.22 and 3.42 MPa sq root of m, respectively. The fatigue crack growth behavior changed from Class-IIb to Class-IIa with increasing fatigue crack growth rate.

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Document Details

Document Type
Technical Report
Publication Date
Oct 02, 1996
Accession Number
ADA321865

Entities

People

  • Eun U. Lee

Organizations

  • Naval Air Warfare Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerial Warfare
  • Aircraft Landings
  • Aircrafts
  • Alloys
  • Aluminum Alloys
  • Chemical Composition
  • Classification
  • Cracks
  • Environment
  • Fatigue Tests (Mechanics)
  • Intensity
  • Landing Gear
  • Materials
  • Materials Testing
  • Nitrogen
  • Resistance
  • Tensile Strength

Readers

  • Materials Science (Mechanical Engineering).