| [1] AIAA Technical Committee for MDO. Current state of the art: multidisciplinary design optimization. Washington D.C.: AIAA White Paper. ISBN 1-56347-021-7, 1991.[2] Kroo I, Altus S, Braun R, et al. Multidisciplinary optimization methods for aircraft preliminary design. AIAA-1994-4325, 1994.[3] Sangook J, Young-Hee J, Rho A J, et al. Application of collaborative optimization using response surface methodology to an aircraft wing design. AIAA-2004-4442, 2004.[4] Guo J. Research on multidiscipline design optimization. Xi'an: College of Astronautics, Northwestern Polytechnical University, 2001. (in Chinese) 郭健. 多学科设计优化技术研究. 西安: 西北工业大学航天学院, 2001.[5] Han M H, Deng J T. Improvement of collaborative optimization. Chinese Journal of Mechanical Engineering, 2006, 42(11): 34-38. (in Chinese) 韩明红, 邓家禔. 协同优化算法的改进. 机械工程学报, 2006, 42(11): 34-38.[6] Yin Z Y, Mi D, Wu L Q, et al. Study on multidisciplinary design optimization of aero-engine. Engineering Science, 2007, 9(6): 1-10. (in Chinese) 尹泽勇, 米栋, 吴立强, 等. 航空发动机多学科设计优化技术研究. 中国工程科学, 2007, 9(6): 1-10.[7] Wang R Q, Jia Z G, Yang J J, et al. Study on disk and blade design based on multi-layer optimization strategy. Journal of Aerospace Power, 2012, 27(6): 1201-1209. (in Chinese) 王荣桥, 贾志刚, 杨俊杰, 等. 基于多层优化策略的涡轮盘叶设计研究. 航空动力学报, 2012, 27(6): 1201-1209.[8] Kaufman M, Balabanov V, Giunta A A, et al. Variable-complexity response surface approximations for wing structural weight in HSCT design. Computational Mechanics, 1996, 18(2): 112-126.[9] Singh G, Grandhi R V. Mixed-variable optimization strategy employing multifidelity simulation and surrogate models. AIAA Journal, 2010, 48(1): 215-223.[10] Baker M L, Munson M J, Alston K Y, et al. Integrated hypersonic aeromechanics tool. AIAA-2003-6952, 2003.[11] Livne E, Navarro I. Nonlinear equivalent plate modeling of wing-box structures. Journal of Aircraft, 1999, 36(5): 851-865.[12] MacMillin P E. Trim, control, and performance effects in variable-complexity high-speed civil transport design. Blacksburg, VA: School of Aerospace Engineering, Virginia Polytechnic Institute and State University, 1996.[13] Robinson T D, Eldred M S, Willcox K E, et al. Surrogate-based optimization using multifidelity models with variable parameterization and corrected space mapping. AIAA Journal, 2008, 46(11): 2814-2822.[14] Wang R Q, Jia Z G, Fan J, et al. Hexahedral mesh regeneration method for MDO on complex aero-engine components. Journal of Aerospace Power, 2011, 26(9): 2032-2038. (in Chinese) 王荣桥, 贾志刚, 樊江, 等. 复杂构件MDO六面体网格重构方法. 航空动力学报, 2011, 26(9): 2032-2038. |
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