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A fatigue crack growth model considering in-plane constraint effects

  • Beihang University
  • Beijing Key Laboratory of Aero-Engine Structure and Strength

科研成果: 期刊稿件文章同行评审

摘要

Fatigue crack growth rates are influenced by constraint effects. However, existing research has failed to provide a consistent conclusion regarding the influence of in-plane constraints on fatigue crack growth behavior. In this study, we present a comprehensive analysis of the effect of in-plane constraint on fatigue crack growth rates. Then, a fatigue crack growth model based on two-parameter fracture mechanics is proposed. The effective stress intensity factor range is defined as ΔKα = ΔK(1 + A3b), where b is a geometric influence factor that measure the extent to which geometry affects crack growth rates, A3 is the third term in Williams series expansion. Experimental validation showed that our model could describe the constraint effect on the fatigue crack growth rates under conditions where Cm exhibits a monotonically increasing relationship with A3.

源语言英语
文章编号111052
期刊Engineering Fracture Mechanics
320
DOI
出版状态已出版 - 13 5月 2025

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