Unusual Fatigue Crack Growth Behavior of Long Cracks at Low Stress Intensity Factor Ranges

Author:

Kujawski Daniel1,Vasudevan Asuri K.2

Affiliation:

1. Mechanical and Aerospace Engineering, Western Michigan University, Kalamazoo, MI 49008, USA

2. TDA Inc., Falls Church, VA 22043, USA

Abstract

In this article, we characterize and review the unusual lack of threshold in fatigue crack growth (FCG) behavior for some alloys at low values of stress intensity factor ranges ΔK and its implications to damage-tolerant design approaches. This unusual behavior was first observed by Marci in 1996 in IMI 834 alloy. Conventional applications of linear elastic fracture mechanics to FCG analysis at constant R-ratio (or Kmax) assumes that (da/dN) decreases monotonically with decreasing ΔK and approaches the threshold value of ΔKth with (da/dN) ≤ 10−7 mm/cycle for a given R (or Kmax). However, instead of ΔK threshold behavior, some materials exhibit plateau or acceleration in da/dN rate with decreasing ΔK for long cracks tested in both constant R and Kmax conditions. This unusual (da/dN)-ΔK behavior is only observed experimentally but not understood and represents a challenge to scientists and engineers to model the safe fatigue life prediction of structures under low amplitude vibrating loads.

Publisher

MDPI AG

Reference22 articles.

1. (2015). Standard Test Method for Measurement of Fatigue Crack Growth Rates (Standard No. ASTM E647-15).

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4. The significance of fatigue crack closure;Elber;Damage Tolerance in Aircraft Structures ASTM STP,1971

5. Suresh, S. (2001). Fatigue of Materials, Cambridge University Press. [2nd ed.].

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