Review of Various Hypotheses Used to Correct Notch Elastic Stress/Strain for Local Plasticity

Author(s):  
Shreebanta Kumar Jena ◽  
Punit Arora ◽  
Suneel K. Gupta ◽  
J. Chattopadhyay
Author(s):  
A. Fischersworring ◽  
W. Koschel

The assessment of fatigue-creep life of hot engine components either using conventional safe life design approach or damage tolerant design concepts require the computation and evaluation of the stress-strain-temperature-time cycles corresponding to the operational sequences. For typical jet engine operations the temperature and elastic stress-strain states for an uncooled turbine blade were calculated using finite elements. A primary concern was the aspect of multiaxiality and associated non-proportionality. The results are discussed in regard to multiaxial equivalent damage concepts.


1992 ◽  
Vol 32 (17) ◽  
pp. 1213-1216
Author(s):  
G. Eckert ◽  
W. Pechhold ◽  
M. Schmid

2000 ◽  
Vol 23 (3) ◽  
pp. 257 ◽  
Author(s):  
RC Chaney ◽  
KR Demars ◽  
ML Talesnick ◽  
A Katz ◽  
M Ringel

1980 ◽  
Vol 102 (3) ◽  
pp. 287-293 ◽  
Author(s):  
F. S. Kelley

A method is proposed for ASME Section III fatigue evaluations which can be applied in the elastic or plastic ranges with constant or varying principal stress/strain directions. The generality of the method is demonstrated. For biaxial or triaxial loadings, the method is shown to be more consistent than the Code procedure given in NB-3228.1.


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