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Tensile, fracture toughness, and fatigue crack growth rate properties of zirconium copper

โœ Scribed by W. A. Logsdon; P. K. Liaw

Publisher
Springer-Verlag
Year
1987
Weight
534 KB
Volume
9
Category
Article
ISSN
0931-7058

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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