Predicting fracture and fatigue crack gr
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Bahram Farahmand; Kamran Nikbin
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Article
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2008
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Elsevier Science
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English
โ 349 KB
The safe-life assessment of components requires information such as the plane stress (K c ), plane strain (K Ic ), partthrough fracture toughness (K Ie ), and the fatigue crack growth rate properties. A proposed parametric/theoretical approach, based on an extended Griffith theory is used to derive