2015
DOI: 10.1016/j.jweia.2015.08.001
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Probabilistic optimization of the main cable and bridge deck of long-span suspension bridges under flutter constraint

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Cited by 22 publications
(6 citation statements)
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“…where, again, the summation appearing in ( 19) is carried out via the direct assembly procedure and the explicit expressions of e f can also be obtained via the direct integration. Now, the statement of the discretized problem is to maximize the buckling load P satisfying Equation (15) and subjected to the volumetric constraint (18).…”
Section:   mentioning
confidence: 99%
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“…where, again, the summation appearing in ( 19) is carried out via the direct assembly procedure and the explicit expressions of e f can also be obtained via the direct integration. Now, the statement of the discretized problem is to maximize the buckling load P satisfying Equation (15) and subjected to the volumetric constraint (18).…”
Section:   mentioning
confidence: 99%
“…where i A denote the normalized cross-sectional area at the i th interpolation point contained in the vector A . By multiplying equation ( 23) by T U and then enforcing the condition (15), it leads to:…”
Section: Solution Schemementioning
confidence: 99%
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“…When the attention is focused on one particular bridge type, size optimization is a common area of research; some works consider also materials as design variable, while few works optimize the structural configuration. In particular, reinforced concrete (RC) portal frame bridges [9][10][11], cable stayed bridges [12][13][14] and suspension bridges [15][16][17] have been object of many researches. Concerning beam bridges, the main object of study has been the deck.…”
Section: Generalmentioning
confidence: 99%
“…This discipline requires high computational effort since it combines DO and RA and has been applied to several multidisciplinary areas as automotive (Sinha (2007), Youn et al (2004) or Cid Montoya et al (2015)), naval (Leheta and Mansour (1997)) or civil engineering (Karadeniz et al (2009) or Kusano et al (2015)). Talking about RBDO applied to aeronautical stiffened panels, Hernandez et al (2013) draws a comparison of three RBDO methods in a metallic panel under buckling constraints, Qu and Haftka (2003) performs RBDO using Monte Carlo Simulations (MCS) and a Design Response Surface (DRS) in order to compute the reliability constraints while Díaz et al (2016) compares stochastic expansions with moment-based methods in the RA and genetic with gradient-based algorithms in the DO phase.…”
Section: Introductionmentioning
confidence: 99%