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SPACE INFILL STUDY OF KRIGING META-MODEL FOR MULTI-OBJECTIVE OPTIMIZATION OF AN ENGINE COOLING FAN

机译:发动机冷却风扇多目标优化的Kriging元模型空间填充研究

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The meta-model based optimization is widely used in the aerodynamical design process for rotating machines, and the main industrial cost of such techniques comes from physical evaluations of answers, either by experimental or numerical means. Design of experiment (DoE) with Latin Hypercube sampling has been studied for the design of an automotive fan system for engine cooling. Surrogate models constructed with Kriging and Co-Kriging methods are estimated with the help of a reference numerical model. The objective of the present work is to assess the necessary number of sampling points for the initial DoE for this kind of meta-model method and to study the influence brought by the sample dispersion. The objective being to execute future aerodynamic optimizations at a reduced cost in term of timeframe and CPU effort. Two parameters, camber and chord length were used to investigate geometrical changes and they are completed with a physical parameter which is the flow rate. The optimization should lead to a higher level of performances with given constraints of rotational speed, torque and packaging. A criterion was defined for the initial necessary number of evaluations and the variances for different DoE design were controlled for the sake of comparison. Starting from an initial meta-model, a variance based method was used for further training with additional points. Uncertainties due to lack of information outside the domain led the model to regularly propose new points on the borders, yielding to high sample variance. A genetic-algorithm was employed to explore the final meta-model and to conduct a multi-objective optimization. Results are presented in terms of Pareto Front and are analysed with SOM to understand the relations between factors and objectives. A final optimal design was selected, and proposed to demonstrate the relevancy of the method.
机译:基于元模型的优化已广泛用于旋转机械的空气动力学设计过程中,此类技术的主要工业成本来自对答案的物理评估,无论是通过实验还是数值手段。对于拉丁文Hypercube采样的实验设计(DoE),已经对用于发动机冷却的汽车风扇系统的设计进行了研究。在参考数值模型的帮助下,估计了使用克里格法和共同克里格法构建的替代模型。本工作的目的是为这种元模型方法评估初始DoE所需的采样点数量,并研究样本分散带来的影响。目标是在时限和CPU工作量方面以降低的成本执行未来的空气动力学优化。弯度和弦长这两个参数用于研究几何变化,并且它们以物理参数(即流量)完成。在给定的转速,扭矩和包装约束的情况下,优化应导致更高的性能水平。为初始必要的评估次数定义了一个标准,为了比较,控制了不同DoE设计的差异。从初始元模型开始,使用基于方差的方法对附加点进行进一步的训练。由于缺乏域外信息而导致的不确定性导致该模型定期在边界上提出新的点,从而导致较高的样本方差。遗传算法用于探索最终的元模型并进行多目标优化。结果以帕累托阵线表示,并用SOM进行分析以了解因素与目标之间的关系。选择了最终的最佳设计,并提出以证明该方法的相关性。

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