2020
DOI: 10.1080/0305215x.2019.1705289
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Reliability optimization design for composite laminated plate considering multiple types of uncertain parameters

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Cited by 25 publications
(6 citation statements)
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“…After determining the 1~4 order moments of the triangular fuzzy variable using Equation ( 13), the four statistical moments M 1 ∼ M 4 for triangular fuzzy variable are calculated using Equations ( 8)- (11). Then, the lower and upper bounds of M 1 ∼ M 4 for a triangular fuzzy variable are determined using Equation (12).…”
Section: Moments Calculation For Triangular Fuzzy Variablementioning
confidence: 99%
See 1 more Smart Citation
“…After determining the 1~4 order moments of the triangular fuzzy variable using Equation ( 13), the four statistical moments M 1 ∼ M 4 for triangular fuzzy variable are calculated using Equations ( 8)- (11). Then, the lower and upper bounds of M 1 ∼ M 4 for a triangular fuzzy variable are determined using Equation (12).…”
Section: Moments Calculation For Triangular Fuzzy Variablementioning
confidence: 99%
“…To address the problems of incomplete information or insufficient data for uncertain variables, the use of epistemic uncertainty is proposed. This has been widely applied to the uncertainty analysis and reliability design of engineering products [9][10][11]. Some non-probabilistic uncertainty analysis methods have been proposed to address epistemic uncertainties, and summarized by Beer [12], which includes the interval analysis approach [13,14], the convex model [15,16], the fuzzy set [17,18], and the evidence theory [19][20][21][22].…”
Section: Introductionmentioning
confidence: 99%
“…Carbon fiber-reinforced composites (CFRP) have been widely used in the aerospace industry due to their high specific strength and stiffness, performance design, corrosion resistance, and overall shape [1][2][3][4][5][6]. The stiffened composite structure can reduce the weight of structure due to its own material and structural characteristics, which has a great impact on the weight reduction of modern aircraft.…”
Section: Introductionmentioning
confidence: 99%
“…RBDO problems for composite materials can be solved using a double-loop approach, where the reliability analysis is performed as an inner-loop each time the design variables are updated to assess the reliability constraints (Thompson et al , 2006). However, this can result in a large number of function evaluations, leading to high computational cost (Díaz et al , 2016; Peng et al , 2020; Li et al , 2019). Thus, the double loop approach is usually only computationally feasible when solving the problem using a gradient-based optimisation method, with analytical models (or small numerical models) and an approximate analytical reliability method (e.g.…”
Section: Introductionmentioning
confidence: 99%