Fatigue Life Estimation Using Frequency Domain Technique and Probabilistic Linear Cumulative Damage Model

2021 ◽  
Author(s):  
Diego Burgos ◽  
Vagner Pascualinotto Junior
Keyword(s):  
Fatigue Life ◽  
Frequency Domain ◽  
Damage Model ◽  
Cumulative Damage ◽  
Life Estimation ◽  
Fatigue Life Estimation ◽  
Cumulative Damage Model

scholarly journals Time and frequency domain models for multiaxial fatigue life estimation under random loading

2015 ◽  
Vol 9 (33) ◽  
pp. 376-381 ◽  
Author(s):  
Andrea Carpinteri ◽  
Andrea Spagnoli ◽  
Camilla Ronchei ◽  
Sabrina Vantadori
Keyword(s):  
Fatigue Life ◽  
Frequency Domain ◽  
Multiaxial Fatigue ◽  
Random Loading ◽  
Life Estimation ◽  
Fatigue Life Estimation ◽  
Domain Models

scholarly journals Application of Spectral Method for Vibration-Induced High-Cycle Fatigue Evaluation of an HP Turbine Blade

2020 ◽  
Author(s):  
Iroizan Ubulom
Keyword(s):  
Fatigue Life ◽  
Frequency Domain ◽  
Turbine Blade ◽  
Euler Angle ◽  
Mean Stress ◽  
Critical Plane ◽  
Life Estimation ◽  
Fatigue Life Estimation ◽  
The Mean ◽  
Fully Coupled

Abstract A method of fluid-structure interaction coupling is implemented for a forced-response, vibration-induced fatigue life estimation of a high-pressure turbine blade. Two simulations approaches; a two-way (fully-coupled) and one-way (uncoupled) methods are implemented to investigate the influence of fluidsolid coupling on a turbine blade structural response. The fatigue analysis is performed using the frequency domain spectral moments estimated from the response power spectral density of the two simulation cases. The method is demonstrated in light of the time-domain method of the rainflow cycle counting method with mean stress correction. Correspondingly, the mean stress and multiaxiality effects are also accounted for in the frequency domain spectral approach. In the mean stress case, a multiplication coefficient is derived based on the Morrow equation, while the case of multiaxiality is based on a criterion which reduces the triaxial stress state to an equivalent uniaxial stress using the critical plane assumption. The analyses show that while the vibration-induced stress histories of both simulation approaches are stationary, they violate the assumption of normality of the frequency domain approaches. The stress history profile of both processes can be described as platykurtic with the distributions having less mass near its mean and in the tail region, as compared to a Gaussian distribution with an equal standard deviation. The fully-coupled method is right leaning with positive skewness while the uncoupled approach is left leaning with negative skewness. The directional orientation of the principal axes was also analyzed based on the Euler angle estimation. Although noticeable differences were found in the peak distribution of the normal stresses for both methods, the predicted Euler angle orientations were consistent in both cases, depicting a similar orientation of the critical plane during a crack initiation process. It is shown that the fatigue life estimation was conservative in the fully-coupled solution approach.

scholarly journals Efficient frequency-domain based fatigue life estimation of spot welds in vehicle components

2019 ◽  
Vol 83 (4) ◽  
pp. 921-931
Author(s):  
Milan Zigo ◽  
Eray Arslan ◽  
Werner Mack ◽  
Gerhard Kepplinger
Keyword(s):  
Fatigue Life ◽  
Frequency Domain ◽  
Spot Welds ◽  
Life Estimation ◽  
Fatigue Life Estimation ◽  
Vehicle Components

Frequency domain methods for fatigue life estimation

2021 ◽  
pp. 163-171
Author(s):  
Janko Slavič ◽  
Matjaž Mršnik ◽  
Martin Česnik ◽  
Jaka Javh ◽  
Miha Boltežar
Keyword(s):  
Fatigue Life ◽  
Frequency Domain ◽  
Life Estimation ◽  
Fatigue Life Estimation ◽  
Frequency Domain Methods
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