Creep-fatigue behavior of a new generation Ni-base superalloy for aeroengine usage
Author:
Publisher
Elsevier BV
Subject
Applied Mathematics
Reference21 articles.
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3. Jackson MP., Reed RC. Heat Treatment of Udimet 720Li: The Effect of Microstructure on Properties. Materials Science and Engineering A 1999; 259: 85-97.
4. Baldan A. Combined Effects of Thin-Section Size, Grain Size and Cavities on the High Temperature Creep Fracture Properties of a Nickel Base Superalloy. Journal of Materials Science 1977; 32: 35-45.
5. Brooks RR., Rainforth WM. The Effect of Microstructure on the Morphology of Fatigue Cracks in Udimet 720. Fatigue and Fract. of Eng. Mater. and Structures 2000; 23: 725-736.
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