The Simulation of the Fatigue Fracture Process at Random Loading

Valery V. Nikonov; Vasily S. Shapkin

doi:10.4028/www.scientific.net/KEM.592-593.113

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The Simulation of the Fatigue Fracture Process at Random Loading
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HomeKey Engineering MaterialsKey Engineering Materials Vols. 592-593The Simulation of the Fatigue Fracture Process at...

The Simulation of the Fatigue Fracture Process at Random Loading

Abstract:

The general scheme of crack growth modeling and periodicity of aviation structure elements checks was developed. The major factors determined the scale of inaccuracy calculation ( εN*) based on calculations of crack growth duration (N*) and inspections intervals (τ0) were marked and estimated with the block diagram.

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Periodical:

Key Engineering Materials (Volumes 592-593)

Pages:

113-116

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.592-593.113

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Online since:

November 2013

Authors:

Valery V. Nikonov, Vasily S. Shapkin

Keywords:

Fatigue Crack Growth (FCG), Modeling, Random Cyclic Loads

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References

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