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APPLICATION OF VARIABLE-FIDELITY MODELS TO AERODYNAMIC OPTIMIZATION
作者姓名:夏露  高正红
作者单位:School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, P. R. China
摘    要:For aerodynamic shape optimization, the approximation management framework (AMF) method is used to organize and manage the variable-fidelity models. The method can take full advantage of the low-fidelity, cheaper models to concentrate the main workload on the low-fidelity models in optimization iterative procedure. Furthermore, it can take high-fidelity, more expensive models to monitor the procedure to make the method globally convergent to a solution of high-fidelity problem. Finally, zero order variable-fidelity aerodynamic optimization management framework and search algorithm are demonstrated on an airfoil optimization of UAV with a flying wing. Compared to the original shape, the aerodynamic performance of the optimal shape is improved. The results show the method has good feasibility and applicability.

关 键 词:空气动力学优化  变量保真度  逼近管理框架  AMF
文章编号:10.0007/s10483-006-0809-z
收稿时间:2004-07-06
修稿时间:2005-12-26

Application of variable-fidelity models to aerodynamic optimization
Lu Xia Doctor,Gao Zheng-hong.APPLICATION OF VARIABLE-FIDELITY MODELS TO AERODYNAMIC OPTIMIZATION[J].Applied Mathematics and Mechanics(English Edition),2006,27(8):1089-1095.
Authors:Lu Xia Doctor  Gao Zheng-hong
Institution:School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,P.R.China
Abstract:For aerodynamic shape optimization, the approximation management framework (AMF) method is used to organize and manage the variable-fidelity models. The method can take full advantage of the low-fidelity, cheaper models to concentrate the main workload on the low-fidelity models in optimization iterative procedure. Furthermore, it can take high-fidelity, more expensive models to monitor the procedure to make the method globally convergent to a solution of high-fidelity problem. Finally, zero order variable-fidelity aerodynamic optimization management framework and search algorithm are demonstrated on an airfoil optimization of UAV with a flying wing. Compared to the original shape, the aerodynamic performance of the optimal shape is improved. The results show the method has good feasibility and applicability.
Keywords:aerodynamic optimization  variable-fidelity  approximation management framework
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