| [1] Li W J. Aircraft conceptual/preliminary design. Xi'an: Northwestern Polytechnical University Press, 2005. (in Chinese) 李为吉. 飞机总体设计. 西安: 西北工业大学出版社, 2005.[2] Sensmerier M D, Samareh J R. Automatic aircraft structural topology generation for multidisciplinary optimization and weight estimation. AIAA-2005-1893, 2005.[3] Masonud R R. A framework for preliminary design of aircraft structures based on process information. NASA NAG-1-1716, 1998.[4] Luo M Q, Liu H, Wu Z. Prototype system research on open conceptual aircraft design. Acta Aeronautica et Astronautica Sinica, 2008, 29(4): 954-959. (in Chinese) 罗明强, 刘虎, 武哲. 开放式飞机总体设计环境的原型研究. 航空学报, 2008, 29(4): 954-959.[5] Raymer D P. Aircraft design: a conceptual approach. 3rd ed. Reston: AIAA Inc., 1999.[6] Chen Y C, Song W B, Liu H. Civil aircraft design. Shanghai: Shanghai Jiao Tong University Press, 2010. (in Chinese) 陈迎春, 宋文滨, 刘洪. 民用飞机总体设计. 上海:上海交通大学出版社, 2010.[7] Roskam J. Aircraft design. Ottawa: Roskam Aviation and Engineering Corporation, 1985.[8] Editorial Committee of Aircraft Design Handbook. Airplane design handbook: Book 8, weight balance and control. Beijing: Aviation Industry Press, 1999. (in Chinese) 《飞机设计手册》总编委会. 飞机设计手册 第8册 重量平衡与控制.北京: 航空工业出版社, 1999.[9] Tian Y L, Liu H, Luo M Q. Research on case base of parameterized large civil aircraft. Acta Aeronautica et Astronautica Sinica, 2010, 31(11): 2202-2208. (in Chinese) 田永亮, 刘虎, 罗明强. 参数化大型客机方案实例库研究. 航空学报, 2010, 31(11): 2202-2208.[10] Gu S F. Aircraft conceptual/preliminary design. Beijing: Beihang University Press, 2001. (in Chinese) 顾诵芬. 飞机总体设计. 北京: 北京航空航天大学出版社, 2001.[11] Kulfan B M. Universal parametric geometry representation method. Journal of Aircraft, 2008, 45(1): 142-158.[12] Wang G L, Sun Y D, Wu Z. Rapid uniform aliform component modeling based on parameter in conceptual aircraft design. Acta Aeronautica et Astronautica Sinica, 2002, 23(6): 575-578. (in Chinese) 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. 航空学报, 2002, 23(6): 575-578.[13] Kulfan B M, Bussoletti J E. Fundamental parametric geometry representations for aircraft component shapes. AIAA-2006-6948, 2006.[14] Luo M Q, Feng H C, Liu H, et al. Rapid cabin design and automated scheme adjustment for civil aircraft. Acta Aeronautica et Astronautica Sinica, 2009, 30(1):73-80. (in Chinese) 罗明强, 冯昊成, 刘虎, 等. 民用飞机客舱快速设计及自动化调整. 航空学报, 2009, 30(1): 73-80.[15] Liu H, Wu Z, Wang G L, et al. Implementation of a sketch based approach to conceptual aircraft design synthesis and modeling. Chinese Journal of Aeronautics, 2004, 17(4): 207-214.[16] Luo M Q, Feng H C, Liu H, et al. Rapid wing structure design and automated scheme adjustment for civil aircraft. Journal of Beijing University of Aeronautics and Astronautic, 2009, 35(4): 468-471. (in Chinese) 罗明强, 冯昊成, 刘虎, 等. 民用飞机机翼结构快速设计及自动化调整. 北京航空航天大学学报, 2009, 35(4): 468-471. |
CJA
