Rapid wing structure design and automated scheme adjustment for civil aircraft

[1] 顾诵芬.飞机总体设计[M].北京:北京航空航天大学出版社, 2001 Gu Songfen. Aircraft conceptual preliminary design[M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2001(in Chinese) [2] Leifsson L T. Multidisciplinary design optimization of low-noise transport aircraft . Virginia: Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University, 2006 [3] Wagner T, Valasek J. Comparison of computational methods for stability and control analysis . AIAA Paper 2005-140, 2005 [4] Fidanci M, Miller J R, Strauss D J. Integrating automated multi-disciplinary optimization in preliminary design of non-traditional aircraft . ADA380252, 2000 [5] Roskam J, Anemaat W A. General aviation aircraft design methodology in a PC environment . AIAA Paper 96-5520, 1996 [6] 刘虎.飞机概念设计支持理论与原型系统研究 .北京:北京航空航天大学航空科学与工程学院,2004 Liu Hu. Research on support theory and prototype system for aircraft conceptual design . Beijing:School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, 2004(in Chinese) [7] Raymer D P. Aircraft design: a conceptual approach[M]. 3rd edition. Reston: AIAA Inc, 1999 [8] 王钢林,孙义东,武哲.飞机总体设计中基于参数的类翼面部件快速统一建模[J].航空学报,2002,23(6):575-578 Wang Ganglin, Sun Yidong, Wu Zhe. Rapid uniform aliform component modeling based on parameter in conceptual aircraft design[J]. Acta Aeronautica et Astronautica Sinica, 2002, 23(6):575-578(in Chinese)