Effect of notch on fatigue behaviour of a directionally solidified superalloy at high temperature

Author:

Shi D. Q.1,Hu X. A.1,Wang J. K.2,Yu H. C.3,Yang X. G.1,Huang J.1

Affiliation:

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

2. Key Lab of Complex Aviation System Simulation; Beijing 100076 China

3. Beijing Institute of Aeronautical Materials; Beijing 100095 China

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference15 articles.

1. High temperature fatigue of nickel-based superalloys - A review with special emphasis on deformation modes and oxidation;Pineau;Eng. Fail. Anal,2009

2. Fatigue crack growth mechanisms in superalloys: an overview;Reed;Mater. Sci. Technol.,2009

3. Fatigue behaviour of CMSX2 superalloy [001] single crystals at high temperature I: Low cycle fatigue of notched specimens;Defresne;Mater. Sci. Eng. A,1990

4. High temperature low cycle fatigue and cyclic constitutive relation of MAR-M247 directionally solidified superalloy;Hasebe;Trans ASME,1992

5. Tension-Torsion Multiaxial Low Cycle Fatigue of Mar-M247LC Directionally Solidified Superalloy at Elevated Temperature;Shirafuji;J. Eng. Mater. Technol.,1998

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