NON-ISOTHERMAL FATIGUE CRACK GROWTH IN HASTELLOY-X

Author:

Marchand N. J.,Pelloux R. M.,Ilschner B.

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference33 articles.

1. 2. V. Moreno, D. M. Nissley, and L. S. Lin (1984 ) Creep-fatigue life prediction for engine hot section materials. NASA CR-I744844, Springfield, Va.

2. 3. G. J. Meyers (1982 ) Fracture mechanics criteria for turbine engine hot section components. NASA CR-167896, Springfield, Va.

3. 4. J. M. Larsen, and T. Nicholas (1984 ) Cumulative damage modelling of fatigue crack growth. Proc. AGARD Conf. on Engine Cyclic Durability by Analysis and Testing. Lisse, Netherlands, May 30th-June 6th.

4. 5. C. A. Rau, A. E. Gemma, and G. R. Leverant (1973 ) Thermal-mechanical fatigue crack propagation in nickel- and cobalt-base superalloys under strain-temperature cycles. ASTM STP 520166 -178 .

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