基于偏相关性分析的多设计要求快速优化设计方法  

Fast optimization design with multi-requirements based on the analysis of partial correlation

作　　者：王丹[1] 白俊强[1] 朱军[1] 华俊 孙智伟[1] 

机构地区：[1]西北工业大学航空学院,西安710072 [2]中国航空研究院,北京100012

出　　处：《空气动力学学报》2014年第2期146-153,158,共9页Acta Aerodynamica Sinica

摘　　要：针对飞行器气动外形优化设计中的多设计点、多目标、多工程约束等多设计要求问题,提出了一种新优化设计方法———多设计要求快速优化设计方法。该方法立足于统计学中的偏相关性分析和线性回归理论,通过对设计变量和设计要求进行偏相关性分析,采用线性回归的方法构建设计变量与设计要求之间的转换模型,将多个设计要求转化为对设计变量的约束,从而简化了优化设计模型,减少了优化过程中调用求解器次数,提高了优化效率。利用该方法对RAE 2822和HSNLF(1)-0213翼型进行了多设计要求优化设计算例验证,并将优化结果与Pareto多目标优化方法结果进行对比,结果证明了本文方法的有效性和可靠性。Aiming at aircraft aerodynamic optimization design problems with multi-requirements including multi-designing points,multi-objects and multi-constraints,a new method for optimization design is proposed in this paper：fast optimization design with multi-requirements.The method is established on the partial correlation and linear regression theories which originated from statistics.According to the analysis of partial correlation between design variables and design requirements,some of the requirements are transformed into the constraints of variables through the transformation model established by the linear regression theory,and the optimization result shows that the simpler the optimization model is,the shorter time will be costed in the optimization design.Two multi-requirements optimization design examples have been investigated in this paper,in which the RAE2822and HSNLF（1）-0213are as the initial foils respectively,and the optimization result by the method in this paper are compared with that of the Pareto multi-object method, which verifies the validity and reliability of the method in this paper.

关 键 词：气动优化设计 多设计要求优化方法 优化设计模型 偏相关分析 线性回归分析 

分 类 号：V211.3[航空宇航科学与技术—航空宇航推进理论与工程]