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基于变可信度代理模型的气动优化 被引量:11

Aerodynamic optimization based on multi-fidelity surrogate
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摘要 对于复杂的多设计变量优化设计问题,构造高精度的代理模型需要大量的高可信度样本,并带来巨大的计算量。利用较小的计算代价构建高精度的代理模型具有很强的工程意义。采用Co-Kriging方法,基于两组相互独立的高、低可信度模型样本,构建了一种高效的变可信度代理模型。Co-Kriging变可信度代理模型通过构建高、低可信度模型之间的关系模型,充分利用低可信度模型信息来提高代理模型整体的预测精度,在保证预测精度的前提下,大大减少了构造代理模型所需的计算时间。使用两个函数算例分析了不同选样方案对近似精度的影响,并用一个基于不同代理模型的RAE2822气动优化设计的对比证明了该方法在工程设计优化中的可行性。 Constructing surrogate models need lots of high-fidelity sample data in complex multivariable simulation-based design optimization problems, and the calculation is very costly. Thereby constructing higher accuracy surrogate model with lower computational cost has great engineering significance. In this paper Co-Kriging method is used to construct multi-fidelity surrogate model based on two independent sample datasets. Thus a greater quantity of low-fidelity information can be used to enhance the accuracy of the highfidelity surrogate model by formulating a form of correction process which reflects the differences between the low and high fidelity model, and the total computational cost of sample data can be greatly reduced. Two function examples demonstrated the influence of approximate accuracy of sample number, and the feasibility of this methodology in engineering design problem is validated by a comparison of different surrogate model based aerodynamic optimization design of RAE2822.
出处 《空气动力学学报》 CSCD 北大核心 2013年第6期783-788,共6页 Acta Aerodynamica Sinica
基金 欧盟委员会和中华人民共和国工业与信息化部联合资助的民用飞机国际合作专项"基于雷诺应力控制的流动分离和减阻研究"
关键词 Co—Kriging 代理模型 变可信度 气动优化 Co-Kriging surrogate model multi-fidelity aerodynamic optimization
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参考文献15

  • 1IKJIN LEE,CHOI K K,ZHAO L. Sampling-based RB DO using the dynamic Kriging (D-Kriging) method and stochastic sensitivity analysis[AIAA 2010-9036][A].Fort Worth,Texas,2010.
  • 2ALLAIRE D,WILLCOX K. Surrogate modeling for uncertainty assessment with application to aviation environmental system models[J].{H}AIAA Journal,2010,(08):1791-1803.
  • 3阎平凡;张长水.人工神经网络与模拟进化计算[M]{H}北京:清华大学出版社,2005.
  • 4BUHMAN N,MARTIN D. Radial basis functions:theory and implementations[M].{H}Cambridge University Press,2003.
  • 5SACKS J,WELCH W J,MICHELL T J,WYNN H P. Design and analysis of computer experiments[J].Statistical Science,1989,(04):409-435.
  • 6GIBBS M N.Bayesian Gaussian processes for regression and classification[D]{H}剑桥大学,1997.
  • 7MYERS R,MONTGOMERY D. Response surface methodology[M].{H}New York:John Wiley and Sons,Inc,1995.
  • 8ZIMMERMANNL R,GORTZ S. Non-linear reduced order models for steady aerodynamics[J].Procedia Computer Science,2010.165-174.
  • 9LEIFSSON L,KOZIEL S. Multi-fidelity design optimization of transonic airfoils using physics-based surrogate modeling and shape-preserving response prediction[J].Journal of Computational Science,2010,(01):98-106.
  • 10DANIEL M J,GEOFFREY T P,WILLIAM N D. Robust multi-fidelity aerodynamic design optimization using surrogate models[AIAA 2008-6052][R].

二级参考文献12

  • 1ANDERSONJD.汁算流体力学基础及应用[M].吴颂平,刘赵淼,译.北京:机械工业出版社,2007.
  • 2王明亮. 飞行器气动与隐身综合设计研究[R]. 西安: 西北工业大学航空学院, 2009.
  • 3WANG J J H. Generalized moment methods in electromagnetics[M]. New York: John Wiley Sons Inc, 1990.
  • 4WANG G, GARY, SHAN S. Review of metamodeling techniques in support of engineering design optimization[J]. ASME Journal of Mechanical Design, 2007, 129(4): 370-380.
  • 5SHAN S Q. Survey of modeling and optimization strategies for high dimensional design problems[A]. 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference[C]. AIAA 2008-5842, 2008.
  • 6MARTIN J D, SIMPSON T W. Use of kriging models to approximate deterministic computer models[J]. AIAA Journal, 2005, 43(4): 853-863.
  • 7SIMPSON T W, PEPLINSKI J D, KOCH P N, et al. Metamodels for computer based engineering design: survey and recommendations[J]. Engineering with Computers, 2001, 17(2): 129-150.
  • 8KULFAN B M. Universal parametric geometry representation method[J]. Journal of aircraft, 2008, 45(1): 142-158.
  • 9DALBEY K R, KARYSTINOS G N. Fast generation of spacefilling latin hypercube sample designs[R]. AIAA 2010-9085, 2010.
  • 10高正红,王明亮.An Efficient Algorithm for Calculating Aircraft RCS Based on the Geometrical Characteristics[J].Chinese Journal of Aeronautics,2008,21(4):296-303. 被引量:5

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