Citation: | XIA Lu, GAO Zheng-hong. Application of Variable-Fidelity Models to Aerodynamic Optimization[J]. Applied Mathematics and Mechanics, 2006, 27(8): 947-953. |
[1] |
Alexandrov N M, Lewis R M, Gumbert C R,et al.Optimization with variable-fidelity models applied to wing design[R]. AIAA,2000—0841.
|
[2] |
施光燕,董加礼.最优化方法[M].北京:高等教育出版社,2000.
|
[3] |
袁亚湘,孙文瑜.最优化理论与方法[M].北京:科学出版社,1999.
|
[4] |
Alexandrov N M,Dennis J E Jr,Lewis R M,et al.A trust-region framework for managing the use of approximation models in optimization[J].Structural Optimization,1998,15(1):16—23. doi: 10.1007/BF01197433
|
[5] |
Booker A J, Dennis J E Jr, Frank P D,et al.A rigorous framework for optimization of expensive functions by surrogates[J].Structural Optimization,1999,17(1): 1—13. doi: 10.1007/BF01197708
|
[6] |
Chang K J,Haftka R T, Giles G L,et al.Sensitivity-based scaling for approximating structural response[J].Journal of Aircraft,1993,30(2):283—288. doi: 10.2514/3.48278
|
[7] |
夏露.飞行器外形气动、隐身综合优化设计方法研究[D].博士学位论文.西安:西北工业大学,2004.
|
[8] |
Hicks R, Henne P. Wing design by numerical optimization[J].Journal of Aircraft,1978,15(7):407—413. doi: 10.2514/3.58379
|