Abstract

Cyclic creep strain is often observed in power equipment parts, especially in gas-turbine rotor blades subjected to the complex action of static and alternating loads over a wide frequency range at high temperature [1-5]. Since the cyclic component of the load has a marked effect on creep rate, and consequently on the endurance of the part and the whole strucure [2-4], considerable attention is de ~ted to studying this process,

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