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Combining Clustered Adaptive Multistart and Discrete Dynamic Convexized Method for the Max-Cut Problem
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作者 Geng Lin Wenxing Zhu 《Journal of the Operations Research Society of China》 EI 2014年第2期237-262,共26页
Given an undirected graph with edge weights,the max-cut problem is to find a partition of the vertices into twosubsets,such that the sumof theweights of the edges crossing different subsets ismaximized.Heuristics base... Given an undirected graph with edge weights,the max-cut problem is to find a partition of the vertices into twosubsets,such that the sumof theweights of the edges crossing different subsets ismaximized.Heuristics based on auxiliary function can obtain high-quality solutions of the max-cut problem,but suffer high solution cost when instances grow large.In this paper,we combine clustered adaptive multistart and discrete dynamic convexized method to obtain high-quality solutions in a reasonable time.Computational experiments on two sets of benchmark instances from the literature were performed.Numerical results and comparisons with some heuristics based on auxiliary function show that the proposed algorithm is much faster and can obtain better solutions.Comparisons with several state-ofthe-science heuristics demonstrate that the proposed algorithm is competitive. 展开更多
关键词 MAX-CUT Local search Dynamic convexized method Clustered adaptive multistart
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基于热阻模型的低雷诺数顺排圆形微针肋热沉多目标优化设计 被引量:2
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作者 杨晨光 邵宝东 +1 位作者 王丽凤 杨洋 《应用力学学报》 CAS CSCD 北大核心 2019年第3期603-609,759-760,共8页
利用离散方法建立了顺排圆形微针肋的离散热阻模型,根据文献结果选取适用于微尺度柱群绕流的压降控制函数,以减小热阻-压降为优化目标构建加权评价函数。通过MultiStart-Fmincon多目标优化算法,对层流状态下顺排圆形微针肋热沉的微柱间... 利用离散方法建立了顺排圆形微针肋的离散热阻模型,根据文献结果选取适用于微尺度柱群绕流的压降控制函数,以减小热阻-压降为优化目标构建加权评价函数。通过MultiStart-Fmincon多目标优化算法,对层流状态下顺排圆形微针肋热沉的微柱间距、半径、宽度进行了优化设计,得到了不同权重下的尺寸优化结果,并用有限元分析软件对优化结果进行了模拟验证。结果表明,在选取的设计区间及工作环境下,本文提出的优化设计方法具有较好的合理性和精度。流场分析表明,柱间流速与过流截面积相关,迎水柱前后的流体压差较大且随微柱集度增加而增大,可通过二次设计提升迎水柱强度。 展开更多
关键词 多目标优化 热阻网络 微针肋热沉 数值模拟 多起点搜索法
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Flutter analysis of an airfoil with multiple nonlinearities and uncertainties
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作者 Haitao Liaon Ge Gao 《Propulsion and Power Research》 SCIE 2013年第3期208-213,共6页
An original method for calculating the limit cycle oscillations of nonlinear aeroelastic system is presented.The problem of detemining the maximum vibration amplitude of limit cycle is transfomed into a nonlinear opti... An original method for calculating the limit cycle oscillations of nonlinear aeroelastic system is presented.The problem of detemining the maximum vibration amplitude of limit cycle is transfomed into a nonlinear optimization problem.The hamonic balance method and the Floquet theory are selected to construct the general nonlinear equality and inequality constraints.The resulting constrained maximization problem is then solved by using the MultiStart algorithm.Finally,the proposed approach is validated and used to analyse the limit cycle oscillations of an airfoil with multiple nonlinearities and uncertainties.Numerical examples show that the coexistence of multiple nonlinearities may lead to low amplitude limit cycle oscillation. 展开更多
关键词 Limit cycle Harmonic balance method Floquet theory The multistart algorithm
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