Experimental investigation on low cycle fatigue and fracture behaviour of a notched Ni-based superalloy at elevated temperature

Author:

Yuan S. H.12,Wang Y. R.12,Wei D. S.12

Affiliation:

1. School of Energy and Power Engineering; Beihang University; Beijing 100191 China

2. Co-Innovation Center for Advanced Aero-Engine; Beihang University; Beijing 100191 China

Funder

the National Natural Science Foundation of China

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference29 articles.

1. Pfouts , W. R. Shamblen , C. E. Mosier , J. S. Peebles , R. E. Gorsler , R. W. 1979 Materials for advanced turbine engines, Volum 1: powder metallurgy Rene95 rotating turbine engine parts NASA-CR-159802

2. Wilbers , L. G. Redden , T. K. 1981 Powder metallurgy Rene95 rotating turbine engine parts 2 NASA-CR-165142

3. Microstructure, properties and heat treatment process of powder metallurgy superalloy FGH95;Guo;J. Iron Steel Res. Int.,2006

4. Progress in structural materials for aerospace systems;Williams;Acta Mater.,2003

5. Tensile and low cycle fatigue properties of nickel-base powder metallurgy superalloy FGH95;Cui;Rare Met. Mater. Eng.,2007

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