Theoretical-Experimental Model for Predicting Crack Growth Rate in Structural Alloys of Aircraft Gas Turbine Engine Disks with Regard to Fatigue and Creep

Author： Pokrovskii V.   Ezhov V.   Sidyachenko V.  

Publisher： Springer Publishing Company

ISSN： 0039-2316

Source： Strength of Materials, Vol.37, Iss.6, 2005-11, pp. : 558-565

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