Fatigue limit--material property as an opened or closed system? Practical view on the aircraft components failures in GCF area (Q2433364)
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scientific article
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Fatigue limit--material property as an opened or closed system? Practical view on the aircraft components failures in GCF area |
scientific article |
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Fatigue limit--material property as an opened or closed system? Practical view on the aircraft components failures in GCF area (English)
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27 October 2006
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gigacycle fatigue
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synergetic
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bifurcation
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aircraft components
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quantitative fractography
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failure analyses
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lifetime to failure
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crack growth period
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0.7497157454490662
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0.7380474805831909
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0.722695529460907
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0.7132099270820618
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0.7096834182739258
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