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

V. V. Pokrovskii، نويسنده , , V. N. Ezhov and V. G. Sidyachenko ، نويسنده ,

روزنامه با شماره پیاپی سال 2005

8

558

565

trapezoidal cyclic loading - crack - hypothesis of linear summation of damages - empirical approaches

Strength of Materials

2005

Strength of Materials

343841