期刊文献+

自适应Kriging近似模型及其在二维扩压器优化设计中的应用 被引量:9

Application of adaptive Kriging approximation model in two dimensional diffuser aerodynamic optimization design
下载PDF
导出
摘要 将均匀设计方法、CFD技术、Kriging近似模型及小生境微种群遗传算法相结合发展了一种自适应全局优化设计方法。优化过程中综合考虑Kriging模型的预测值与预测标准差,引入了EI(Expected Improvement)函数得到校正点,解决了采用近似模型最优策略得到校正点带来的局部收敛问题。分别采用该方法和小生境微种群遗传算法进行扩压器气动优化设计,以扩压器平均静压恢复系数为目标函数并采用Nurbs曲线完成几何参数化建模。优化后扩压器平均静压恢复系数提高了8.5%,结果表明本文方法比随机性优化算法更为有效。 An adaptive global optimization method was developed coupled with uniform experimental design,CFD analysis,Kriging approximation model and niching micro genetic algorithm.In the optimization procedure,EI function was introduced to identify the next sampled point by considering the prediction and mean squared error of Kriging model to decrease the risk of trapping into the local optimum when the optimal strategy was used.The proposed method and niching micro genetic algorithm have been applied to the diffuser optimization design respectively,average static pressure recovery coefficient is selected as objective function and Nurbs curve is used to parameterize the geometric model.8.5% improvement of average static pressure recovery coefficient is obtained and the result shows that the method is more effective than stochastic optimization algorithm.
出处 《计算力学学报》 EI CAS CSCD 北大核心 2011年第1期15-19,24,共6页 Chinese Journal of Computational Mechanics
基金 国家自然科学基金(50576052) 博士点基金(20060248036)资助项目
关键词 扩压器 全局优化 KRIGING模型 试验设计方法 diffuser global optimization kriging model experimental design method
  • 相关文献

参考文献13

  • 1Zhang W L, Knight D D, Smith D. Automated design of a three-dimensional subsonic diffuser[J].Journal of Propulsion and Power, 2000, 16 (6) : 1132-1140.
  • 2Marjavaara B D, Lundstrom T S, Goel T,et al. Hydraulic turbine diffuser shape optimization by multi- ple surrogate model approximations of pareto fronts [J]. Journal of Fluids Engineering, 2007,129 (9) : 1228-1240.
  • 3Oyama A, Liou M S, Obayashi S. Transonic axial flow blade optimization: Evolutionary algorithms/ three dimensional Navier-Stokes solver [J]. Journal of Propulsion and Pozoer ,2004,20( 4) :612-619.
  • 4高行山,韩永志,张娟,邓子辰.基于近似技术的涡轮叶片气动优化设计[J].计算力学学报,2008,25(6):874-877. 被引量:8
  • 5穆雪峰,姚卫星,余雄庆,刘克龙,薛飞.多学科设计优化中常用代理模型的研究[J].计算力学学报,2005,22(5):608-612. 被引量:152
  • 6席光,王志恒,王尚锦.叶轮机械气动优化设计中的近似模型方法及其应用[J].西安交通大学学报,2007,41(2):125-135. 被引量:45
  • 7Lophaven S N,Nielsen H B,Sondergaard J. DACE-A Matlab Kriging Toolbox, version 2. 0 [OL]. http://www2, imm. dtu. dk/-hbn/dace/dace, pdf.
  • 8Carroll D L. Genetic algorithms and optimizing chemical oxygen-iodine lasers[J]. Developments in Theoretical and Applied Mechanics, 1996, 18 (3): 411- 424.
  • 9Bonaiuti D, Arnone A, Ermini M. Analysis and optimization of transonic centrifugal compressor impellers using the design of experiments technique[J]. Journal of Turbomachinery , 2006.128(4) : 786-797.
  • 10Lee J W, Min B Y, Byun Y H, et al. Multipoint nose shape optimization of space launcher using response surface method[J]. Journal of Spacecraft and Rockets, 2006,43(1): 137-146.

二级参考文献40

共引文献201

同被引文献67

引证文献9

二级引证文献40

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部