An Energy Criterion for Low-Cycle Fatigue

1961 ◽  
Vol 83 (4) ◽  
pp. 565-571 ◽  
Author(s):  
D. E. Martin

A criterion for low-cycle fatigue is developed which supposes that the segment of strain hysteresis associated with work-hardening is a measure of damage. On the basis of this “damage” work criterion and assuming a linear work-hardening law, the well-known plastic strain-cyclic life equation, N1/2Δεp = C is derived. The constant C in this equation is evaluated by setting the total damage energy absorbed in N cycles equal to the damage work of a static tensile test. This method of predicting the constant C is in much better agreement with room-temperature strain-cycling data than the previously suggested method of plotting the fracture ductility at 1/4 cycle.

1990 ◽  
Vol 61 (7) ◽  
pp. 325-332 ◽  
Author(s):  
Shree Ram Mediratta ◽  
Vaidyanath Ramaswamy ◽  
Vakil Singh ◽  
Rama Rao

1966 ◽  
Vol 88 (4) ◽  
pp. 801-810 ◽  
Author(s):  
Kiyotsugu Ohji ◽  
W. R. Miller ◽  
Joseph Marin

By assuming a linear cumulative damage hypothesis for strain cycling, theories are developed in this paper for fatigue life under varying strain amplitude, residual ductility after a given history of strain cyling, and life under mean strain condition. These predictions are based on uniaxial completely reversed cycling behavior. The expressions obtained were compared with the experimental results on 2024-T351 aluminum alloy as well as other data available in the literature. The agreements between theories and experiments were found to be satisfactory.


1998 ◽  
Vol 64 (622) ◽  
pp. 1443-1448 ◽  
Author(s):  
Kazuhiro MORINO ◽  
Futoshi NISHIMURA ◽  
Shinichi YAMAMOTO ◽  
Hironobu NISITANI

2006 ◽  
Vol 127 (4) ◽  
pp. 54-60
Author(s):  
Lucjan WITEK

This paper presents results of the stress and fatigue analysis of the turbine disc and blade. A non-linear finite element method was utilized to determine the stress state of the turbine components under operational condition. A critical, high stress zones were found at the several region of turbine. Results obtained from the preliminary static calculation were next used into total fatigue life (S-N) analysis performed for the load time history equivalents to 1-hours work of engine under operating flight. In this analysis, the number of hours to the total damage of the critical components of turbine subjected to low cycle fatigue was estimated.


2001 ◽  
Vol 2001.39 (0) ◽  
pp. 21-22
Author(s):  
Kazuhiro MORINO ◽  
Naohiro SUMIMURA ◽  
Futoshi NISHIMURA ◽  
Hironobu NISITANI

1991 ◽  
Vol 113 (2) ◽  
pp. 102-108 ◽  
Author(s):  
H. D. Solomon

This paper describes the 35°C and 150°C low cycle fatigue behavior of Sn96 solder (96.5 Sn/3.5 AG), the tin silver eutectic. There is a considerable amount of anecdotal information which says that this solder is superior to eutectic solder in its fatigue resistance. This study generally supports this assertion, but not for all plastic strain ranges. This solder has an excellent balance of strength, ductility and fatigue life under strain cycling. Furthermore, it is also shown that this solder is superior to a high Pb solder (92.5 Pb/2.5 Ag/5.0 Sn). The only drawback of the tin silver eutectic is that it has a higher melting point than the melting point for the Sn/Pb eutectic (221°C versus 183°C), and this requires a higher soldering temperature. This higher temperature necessitates some process alterations in order to use this solder.


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