Meta model-based global design optimization and exploration method

被引:0
作者
Guo, Zhen-Dong [1 ]
Song, Li-Ming [1 ]
Li, Jun [1 ]
Li, Guo-Jun [1 ]
Feng, Zhen-Ping [1 ]
机构
[1] School of Energy & Power Engineering, Xi'an Jiaotong University, Xi'an
来源
Tuijin Jishu/Journal of Propulsion Technology | 2015年 / 36卷 / 02期
关键词
Data mining; Global optimization; Kriging model; Meta-modeling;
D O I
10.13675/j.cnki.tjjs.2015.02.007
中图分类号
学科分类号
摘要
To solve computationally expensive black box problem such as turbomachinery design optimization in an effective way, a meta-model based global design optimization and exploration method named MBOE is proposed by integrating a meta-model based global optimization algorithm named MBGO and data mining techniques. The MBGO algorithm can usually achieve the global optimum with minimum function evaluations. Data mining techniques provide a way to get insights into the interactions among parameters and uncover the mechanism behind performance improvement of the optimal design. Using MBOE, 3D design optimization and data mining of Rotor 37 blade are finished. Isentropic efficiency of the optimal design is 1.74% higher than that of the reference design. And the computing time of MBGO is just 1/5 of that by applying a modified differential evolution algorithm as the optimizer. Meanwhile, data mining results indicate that the leading edge and the 3D stacking style have great effect on the blade aerodynamic performance. The performance improvement of the optimal design is benefited from the changes of related parameters. Therefore, the correctness and effectiveness of MBOE method is demonstrated. ©, 2015, Editorial Department of Journal of Propulsion Technology. All right reserved.
引用
收藏
页码:207 / 216
页数:9
相关论文
共 20 条
[1]  
Shan S., Wang G.G., Survey of Modeling and Optimization Strategies to Solve High-Dimensional Design Problems with Computationally-Expensive Black-Box Functions, Structural and Multidisciplinary Optimization, 41, 2, pp. 219-241, (2010)
[2]  
Oyama A., Liou M.S., Obayashi S., Transonic Axial-Flow Blade Optimization: Evolutionary Algorithms/Three-Dimensional Navier-Stokes Solver, Journal of Propulsion and Power, 20, 4, pp. 612-619, (2004)
[3]  
Lian Y., Liou M.S., Multi-Objective Optimization of Transonic Compressor Blade Using Evolutionary Algorithm, Journal of Propulsion and Power, 21, 6, pp. 979-987, (2005)
[4]  
Okui H., Verstraete T., Van Den Braembussche R.A., Et al., Three-Dimensional Design and Optimization of a Transonic Rotor in Axial Flow Compressors, Journal of Turbomachinery, 135, 3, (2013)
[5]  
Jones D.R., Schonlau M., Welch W.J., Efficient Global Optimization of Expensive Black-Box Functions, Journal of Global optimization, 13, 4, pp. 455-492, (1998)
[6]  
Jeong S., Obayashi S., Efficient Global Optimization (EGO) for Multi-Objective Problem and Data Mining, Evolutionary Computation, 3, pp. 2138-2145, (2005)
[7]  
Simpson T.W., Toropov V., Balabanov V., Et al., Design and Analysis of Computer Experiments in Multidisciplinary Design Optimization: a Review of How Far we Have Come or Not
[8]  
Jeong S., Chiba K., Obayashi S., Data Mining for Aerodynamic Design Space, Journal of Aerospace Computing, Information, and Communication, 2, 11, pp. 452-469, (2005)
[9]  
Oyama A., Nonomura T., Fujii K., Data Mining of Pareto-Optimal Transonic Airfoil Shapes Using Proper Orthogonal Decomposition, Journal of Aircraft, 47, 5, pp. 1756-1762, (2010)
[10]  
Luersen M.A., Le Riche R., Guyon F., A Constrained, Globalized, and Bounded Nelder-Mead Method for Engineering Optimization, Structural and Multidisciplinary Optimization, 27, 1-2, pp. 43-54, (2004)