Statistics of Crack Growth in Engine Materials. Volume 1. Constant Amplitude Fatigue Crack Growth at Elevated Temperatures

Abstract

Classically crack propagation analyses for engine components employed in residual life predictions are deterministically based. They typically account for materials scatter by the incorporation of a safety factor. A statistical treatment of materials scatter is necessary to permit a maximum utilization of component life. Two fracture mechanics-based statistical models for the fatigue crack growth damage accumulation in engine materials are proposed and investigated. These statistical models are based on the synergistic fracture mechanics models, i.e., hyperbolic sine crack growth rate function, developed by Pratt and Whitney. Test results of IN-100, a superalloy used in the F-100 engine, at various elevated temperatures, loading frequencies, stress ratios, etc., have been compiled and analyzed statistically. The statistical distributions of (1) the crack growth rate; (2) the propagation life to reach any given crack size; and (3) the crack size at any service life, have been derived. It is demonstrated that the correlation between the test results and two statistical models is very good.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1982
Accession Number
ADA119607

Entities

People

  • C. G. Annis Jr.
  • G. C. Salivar
  • J. N. Yang

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • C4I

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Databases
  • Distribution Functions
  • Engine Components
  • Engineering
  • Fracture (Mechanics)
  • Information Science
  • Materials Laboratories
  • Mechanics
  • Normal Distribution
  • Probability
  • Probability Density Functions
  • Random Variables
  • Statistical Analysis
  • Statistical Distributions
  • Turbines

Readers

  • Regression Analysis.
  • Structural Health Monitoring of Composite Structures.