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Multi-objective shape optimization using ant colony coupled computational fluid dynamics solver

机译:蚁群耦合计算流体动力学求解器的多目标形状优化

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An adaptation of a parametric ant colony optimization (ACO) to multi-objective optimization (MOO) is presented in this paper. In this algorithm (here onwards called MACO) the concept of MOO is achieved using the reference point (or goal vector) optimization strategy by applying scalarization. This method translates the multi-objective optimization problem to a single objective optimization problem. The ranking is done using e-dominance with modified L_p metric strategy. The minimization of the maximum distance from the goal vector drives the solution close to the goal vector. A few validation test cases with multi-objectives have been demonstrated. MACO was found to out perform R-NSGA-II for the test cases considered. This algorithm was then integrated with a meshless computational fluid dynamics (CFD) solver to perform aerodynamic shape optimization of an airfoil. The algorithm was successful in reaching the optimum solutions near to the goal vector on one hand. On the other hand the algorithm converged to an optimum outside the boundary specified by the user for the control variables. These make MACO a good contender for multi-objective shape optimization problems.
机译:本文提出了参数化蚁群优化(ACO)对多目标优化(MOO)的适应性。在该算法(以下称为MACO)中,MOO的概念是通过应用标量化使用参考点(或目标向量)优化策略实现的。该方法将多目标优化问题转换为单目标优化问题。使用具有改进的L_p度量策略的电子支配来完成排名。距目标向量的最大距离的最小化使解决方案接近目标向量。已经证明了一些具有多目标的验证测试用例。发现MACO在考虑的测试案例中胜过R-NSGA-II。然后将此算法与无网格计算流体动力学(CFD)求解器集成在一起,以对翼型进行空气动力学形状优化。该算法一方面成功地达到了接近目标向量的最优解。另一方面,该算法收敛到用户为控制变量指定的边界之外的最优值。这些使MACO成为解决多目标形状优化问题的良好竞争者。

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