Experimental Plan for the Development of Equivalent Crack Size Distributions and a Monte Carlo Model of Fatigue in Low and High-kt Specimens of Corroded AA7050-T7451

Abstract

Fatigue life data from low and high-kt specimen are difficult to compare due to the smaller sampling volume of high-kt specimens. As a result, equivalent crack size (ECS) distributions developed using low-kt specimens cannot be used in high-kt conditions such as near fastener holes. This experimental plan addresses this issue for corroded AA7050-T7451. Fatigue crack growth (FCG) and fatigue life tests will be conducted on low and high-kt specimens which have been designed to minimise the differences between the specimens other than the different stress field. FCG data and ECS distributions will be developed for both specimens types. A Monte Carlo model will then be used to test if the low-kt ECS distribution can accurately predict the fatigue lives of the high-kt specimens. If successful, this will allow low-kt ECS distributions, which are easier to derive, to be used under high-kt conditions.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 2012
Accession Number
ADA563803

Entities

People

  • Bruce R. Crawford
  • Chris Loader
  • P. K. Sharp
  • Timothy J. Harrison

Organizations

  • Defence Science and Technology Group

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Air Force Research Laboratories
  • Aircrafts
  • Airframes
  • Computational Science
  • Corrosion
  • Engineering Drawings
  • Fasteners
  • Fatigue Life
  • Fatigue Tests (Mechanics)
  • Fighter Aircraft
  • Life Tests
  • Materials
  • Monte Carlo Method
  • Sampling
  • Simulations
  • Vehicles

Readers

  • Psychological Intervention/Treatment for Stress, Anxiety, PTSD, and Related Emotional and Cognitive Health Symptoms.
  • Structural Health Monitoring of Composite Structures.