Mean vs. Life-Limiting Fatigue Behavior of a Nickel-Based Superalloy (Postprint)

Abstract

The mean and the life-limiting behavior under fatigue of the nickel-based superalloy, IN100, separated (or converged) as a function of stress level and dwell loading. This behavior was related to the control of the life-limiting behavior by the small-crack growth regime, producing its much slower response to stress level and dwell-time, relative to the mean-lifetime behavior. The lifetime probability density is therefore, modeled as a superposition of the crack growth lifetime density and a mean-lifetime density. The crack growth density is calculated with the help of small-crack growth data and the distribution in the crack initiation size. The mean-lifetime density is estimated from a relatively small number of total lifetime fatigue tests. In IN100, we apply this approach to predict the effects of stress level and dwell time on the lifetime distribution and the B0.1 (1 in 1000 probability of failure) lifetime limit.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 2008
Accession Number
ADA503540

Entities

People

  • J. M. Larsen
  • M. J. Caton
  • Shikhar Krishn Jha

Organizations

  • Universal Technology Corporation (United States)

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Air Force Research Laboratories
  • Alloys
  • Dwell Time
  • Electron Microscopes
  • Failure Mode And Effect Analysis
  • Life Cycle Management
  • Manufacturing
  • Materials
  • Microstructure
  • Military Research
  • Particles
  • Probability
  • Probability Density Functions
  • Random Variables
  • Superalloys

Readers

  • Statistical inference.
  • Structural Health Monitoring of Composite Structures.