A Confrontation of Mathematical Models for Fatigue Life with Actual Service Data

Abstract

From a collection of over a thousand different groups of qualified aluminum fatigue data, an empiric distribution is obtained which can serve as a standard for comparison of various mathematical models for fatigue. On this basis several commonly used parametric models, as well as some mathematical suppositions, can be discarded if good predications are desired of the earliest fatigue failures. One of the models not disqualified, which contains sufficient flexibility to fit the actual data, is a distribution of the log-life with three parameters, namely, location, scale and flexure. Because maximum likelihood estimation of all three parameters cannot be accomplished simultaneously, the location parameter is posited as being calculated on the basis of a cumulative damage rule known a priori while the scale parameter is determined from the material and the flexure parameter describes the presence of flaws and/or the time to crack initiation. These relations with the physics of materials provide a design basis for calculation of reliability.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1976
Accession Number
ADA030018

Entities

People

  • Sam C. Saunders

Organizations

  • Washington State University

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Acceptability
  • Air Force
  • Aircrafts
  • Airframes
  • Aluminum Alloys
  • Applied Mathematics
  • Composite Materials
  • Engineering
  • Failure Mode And Effect Analysis
  • Fatigue Life
  • Materials
  • Mathematical Models
  • Mechanics
  • Probability
  • Random Variables
  • Standards
  • Structural Components

Readers

  • Computational Modeling and Simulation
  • Materials Science (Mechanical Engineering).
  • Regression Analysis.