The effect of hold time and waveform on the high-temperature, low-cycle fatigue properties of a Nb-A286 alloy

2001 ◽  
Vol 32 (10) ◽  
pp. 2539-2546 ◽  
Author(s):  
Byung Sup Rho ◽  
Ki Jae Kim ◽  
Soo Woo Nam ◽  
Soo Woo Nam
1983 ◽  
Vol 69 (1) ◽  
pp. 97-106 ◽  
Author(s):  
Masaru YAMAMOTO ◽  
Yasushi HORIUCHI ◽  
Ohmi MIYAGAWA ◽  
Dai FUJISHIRO

2013 ◽  
Vol 577 ◽  
pp. 81-86 ◽  
Author(s):  
Byung Kyu Kim ◽  
Dong-Ik Kim ◽  
In-Suk Choi ◽  
Woo Sang Jung ◽  
Sook In Kwun

2008 ◽  
Vol 30 (3) ◽  
pp. 538-546 ◽  
Author(s):  
G.V. Prasad Reddy ◽  
R. Sandhya ◽  
M. Valsan ◽  
K. Bhanu Sankara Rao

2014 ◽  
Vol 618 ◽  
pp. 120-124
Author(s):  
Yuan Yuan Wang ◽  
Bao Sen Wang ◽  
Li Jia Chen

High temperature low cycle fatigue properties and fracture behavior of Inconel 625 nickel-base superalloy welding joint at 760oC were investigated under fully reversed total strain-controlled mode. The fatigue life and cyclic stress-strain data were analyzed to determine the individual strain fatigue parameters. It is noted that the welding joint exhibits the cyclic strain hardening and stability. The fatigue cracks initiate predominantly on the free surface of fatigue specimens and propagate in an intergranular mode or a mixed transgranular and intergranular mode.


2013 ◽  
Vol 135 (6) ◽  
Author(s):  
Celine Cabet ◽  
Laura Carroll ◽  
Richard Wright

Alloy 617 is the leading candidate material for an intermediate heat exchanger (IHX) application of the very high temperature nuclear reactor (VHTR), expected to have an outlet temperature as high as 950 °C. Acceptance of Alloy 617 in Section III of the ASME Code for nuclear construction requires a detailed understanding of the creep-fatigue behavior. Initial creep-fatigue work on Alloy 617 suggests a more dominant role of environment with increasing temperature and/or hold times evidenced through changes in creep-fatigue crack growth mechanisms and failure life. Continuous cycle fatigue and creep-fatigue testing of Alloy 617 was conducted at 950 °C and 0.3% and 0.6% total strain in air to simulate damage modes expected in a VHTR application. Continuous cycle fatigue specimens exhibited transgranular cracking. Intergranular cracking was observed in the creep-fatigue specimens and the addition of a hold time at peak tensile strain degraded the cycle life. This suggests that creep-fatigue interaction occurs and that the environment may be partially responsible for accelerating failure.


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