2014
DOI: 10.1007/s00170-014-6325-2
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Reliability-based design optimization for fatigue damage analysis

Abstract: The objective of reliability-based design optimization (RBDO) is to design structures which should be both economic and reliable. The existing methods lead to very high computational cost, local optima, and weak convergence stability. In this paper, we present a new methodology of RBDO, leading to global solutions without additional computing cost for the reliability evaluation. The safety factor formulation for linear and nonlinear cases has been used to reduce efficiently the computational time. This techniq… Show more

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Cited by 15 publications
(7 citation statements)
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“…This integration takes into account the randomness of the applied loads and the geometry description. The RBTO problem is generally written as: where β and β t are the reliability index of the system and the target reliability index, respectively (for more information about reliability methods, see 11 [16]). The integration of reliability analysis into the topology optimization has been carried out by performing two decoupled problems for static studies [2].…”
Section: Reliability-based Topology Optimizationmentioning
confidence: 99%
See 1 more Smart Citation
“…This integration takes into account the randomness of the applied loads and the geometry description. The RBTO problem is generally written as: where β and β t are the reliability index of the system and the target reliability index, respectively (for more information about reliability methods, see 11 [16]). The integration of reliability analysis into the topology optimization has been carried out by performing two decoupled problems for static studies [2].…”
Section: Reliability-based Topology Optimizationmentioning
confidence: 99%
“…Considering that the random variable vector follows the normal distribution law, the safety factor can be written as follows 12 [16]:…”
Section: Reliability-based Topology Optimizationmentioning
confidence: 99%
“…The endurance limits for the reversed tension stress and torsion stress f-1 and t-1 stated after 2.106 cycles are equal to 252MPa and 182MPa, respectively. For more details about the fatigue data and methods of this example, the interested reader can refer to [12]. The length and the height of the studied plate are: L=0.14 m and H=0.1 m, respectively (Fig.…”
Section: Numerical Applicationmentioning
confidence: 99%
“…2,3 When the pantograph worked for a period, some cracks were found in the pantograph CHS and the vane where fatigue failure may occur. To ensure the normal usage of pantograph and reduce accident occurrences, it is necessary to investigate the fatigue life and reliability of the pantograph CHS.…”
Section: Introductionmentioning
confidence: 99%