[1] 陈光.航空发动机发展综述.航空宇航制造技术, 2000(6):24-27,34.
[2] 党松.涡轮动叶参数化建模方法研究及系统实现[D].西安:西北工业大学, 2008.
[3] 李卉荟,万学明.涡轮叶片尾缘劈缝冷却结构及具有该冷却结构的涡轮叶片.中国,实用新型专利, 201120545516.6.2012-09-05.
[4] Yong J H, Chen F H. Geometric hermite curves with minimum strain energy.Computer Aided Geometric Design, 2004, 21(3): 281-301.
[5] Leonilde Rocha Varela,Rita Almeida Ribeiro.Evalution of simulated annealing to solve fuzzy optimization problems. Journal of Interlligent & Fuzzy Systems,2003, 14(2):59-71.
[6] Zhang C M, Zhang P F. Fairing curves and surfaces by minimizing energy.Computer Aided Design,2001,33: 913-923. |