Probabilistic Reliability Evaluation of Space System Considering Physics of Failure: Case Study of Fatigue Analysis

Author(s):  
Saeed Kiad ◽  
Mohammad Pourgol-Mohammad ◽  
Hossein Salimi

Mission assurance requires due diligence reliability for space systems taking into account limited accessibility, high uncertainty on the life data and high cost of failure. The methods based on physics of failure are promising approaches for durability evaluation of these systems. In this study, the reliability analysis is aimed for space structures, with the focus on fatigue failure. In this research, the deterministic fatigue simulation is conducted on space systems (satellite in orbit, low-level LEO1, made of aluminum 2024-T3), using models with constant and variable amplitude loading. Walker and Forman models are preliminary utilized in this study for life prediction for benchmarking with the experimental results. In the case of the variable amplitude loading, due to the amount of plastic zone in crack tip, the fatigue crack growth rate will be ceased in case of overload. Deterministic crack growth simulation was numerically simulated by using the MATLAB software and has been compared with commercial AFGROW software for verification and was observed proper match with experimental data. In the analysis of stochastic fatigue crack growth, uncertainty is analyzed by using the Monte Carlo simulation. The universal stochastic crack growth model proposed by Yang and Manning, was used for reliability analysis based on giving probabilistic method for the purpose of power and second polynomial models. In this study, these models are evaluated and three models of I) rational model, II) exponential model and III) global model are proposed. In uncertainty analysis, it is observed that by increasing the crack length, uncertainty range is widening. In case of constant amplitude loading with the same stress intensity factor range but different stress ratio, the uncertainty range was widening with increasing stress ratio. In reliability analysis, the exponential model demands less computational resources however it has a lower accuracy. The fractional model, proposed in this research, is based on the modification to Forman model. However, these models don’t consider geometric factor. The Global model, another model proposed in this research, has the capability of considering this aspect. In multiplicative stochastic factor (Yang and Manning method), accuracy of the approximation is most important. By improving the accuracy of this relation, the result accuracy is enhanced. For this purpose, for increasing efficiency of this method, the accuracy of approximation must be increased by corrections prior models or provide new accurate models.

1976 ◽  
Vol 98 (3) ◽  
pp. 208-212 ◽  
Author(s):  
A. M. Sullivan ◽  
T. W. Crooker

To investigate load sequencing effects in fatigue-crack growth, surface flaw or part-through crack (PTC) specimens of a high-strength pressure vessel steel were subjected to variable-amplitude cyclic loading. Blocks of different load sequences and stress-ratio (R) patterns and cyclic lengths were employed. Crack-growth rate (da/dN) data were analyzed within the framework of linear elastic fracture mechanics using the stress-intensity range parameter, ΔK. The da/dN data were found to correlate well with a seauence-independent formulation of ΔK derived using nominal mean stress, σm, for the loading blocks studied. However, it proved necessary to utilize the normalizing relationship discussed in “Analysis of Fatigue-Crack Growth in a High-Strength Steel—Part I: Stress Level and Stress Ratio Effects at Constant Amplitude”, to account for stress-ratio effects observed under the variable-amplitude block loading. Only the sequential block pattern of high-low-intermediate produced a significant crackgrowth retardation. Predictions made using the sequence-independent normalizing procedure compare favorably with those using the Willenborg model. It is concluded that useful predictions for structural life under variable-amplitude cyclic loading sequences can be made for a wide variety of high-strength pressure vessel applications using sequence-independent analysis procedures.


1978 ◽  
Vol 100 (4) ◽  
pp. 416-420 ◽  
Author(s):  
D. P. Wilhem ◽  
M. M. Ratwani

Crack growth resistance for both static (rising load) and for cyclic fatigue crack growth has been shown to be a continuous function over a range of 0.1 μm to 10 cm in crack extension for 2024-T3 aluminum. Crack growth resistance to each fatigue cycle of crack extension is shown to approach the materials ordinary undirectional static crack resistance value when the cyclic stress ratio is zero. The fatigue crack extension is averaged over many cycles and is correlated with the maximum value of the crack tip stress intensity, Kmax. A linear plot of crack growth resistance for fatigue and static loading data shows similar effects of thickness, stress ratio, and other parameters. The effect of cyclic stress ratio on crack growth resistance for 2219 aluminum indicates the magnitude of differences in resistance when plotted to a linear scale. Prediction of many of these trends is possible using one of several available crack growth data correlating techniques. It appears that a unique resistance curve, dependent on material, crack orientation, thickness, and stress/physical environment, can be developed for crack extensions as small as 0.076 μm (3 μ inches). This wide range, crack growth resistance curve is seen of immense potential for use in both fatigue and fracture studies.


2005 ◽  
Vol 297-300 ◽  
pp. 1120-1125 ◽  
Author(s):  
Myung Hwan Boo ◽  
Chi Yong Park

In order to study the influence of stress ratio and WC grain size, the characteristics of fatigue crack growth were investigated in WC-Co cemented carbides with two different grain sizes of 3 and 6 µm. Fatigue crack growth tests were carried out over a wide range of fatigue crack growth rates covering the threshold stress intensity factor range DKth. It was found that crack growth rate da/dN against stress intensity factor range DK depended on stress ratio R. The crack growth rate plotted in terms of effective stress intensity factor range DKeff still exhibited the effect of microstructure. Fractographic examination revealed brittle fracture at R=0.1 and ductile fracture at R=0.5 in Co binder phase. The amount of Co phase transformation for stress ratio was closely related to fatigue crack growth characteristics.


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