[1] 关振群,顾云宪,张洪武,等. 三维CAD/CAE一体化的参数化动态有限元建模.计算机集成制造系统,2003,9(12):1112-1119.
[2] Chintapalli S. The development of a preliminary structural design optimization method of an aircraft wing-box skin-stringer panels. Aerospace Science and Technology,2010(14):188-198.
[3] Rocca G L, Tooren M J L. A knowledge based engineering approach to support automatic generation of FE models in aircraft design. 45th AIAA Aerospace Sciences Meeting. Reno:AIAA,2007: 967.
[4] Rocca G L, Tooren M J. L. Knowledge-based engineering approach to support aircraft multidisciplinary design and optimization. Journal of Aircraft,2009; 46(6): 1875-1885.
[5] 罗明强,冯昊龙,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.
[6] 朱苏. 基于中间平台的船舶CAD/CAE模型转换研究[D].上海: 上海交通大学,2011.
[7] Sensmeier M, Samareh J. Automatic aircraft structural topology generation for multidisciplinary optimization and weight estimation. 46th AIAA/ASME/ASC Structures and Materials Conference. Austin:AIAA,2005:1893.