[1]  杨锐, 石南林, 王玉敏，等. Sic纤维增强钛基复合材料研究进展[J].钛工业进展, 2005, (5): 37-41.

[2]  李建辉, 李春峰, 雷廷权. 金属基复合材料成形加工研究进展[J].材料科学与工艺, 2002, (2): 207-212.

[3]  张晓明, 刘雄亚. 纤维增强热塑性复合材料及其应用[M]. 北京: 化学工业出版社, 2007.

[4]  Mallon P J, OBradaigh C M, Pipes R B. Polymeric diaphragm forming of continuous fiber reinforced thermoplastics[A]. Proc. 33rd Internatl. SAMPE Symp.[C]. Anaheim, CA, 1988.

[5]  Monaghan M R, OBradaigh C M, Mallon P J,  et al. The effect of diaphragm stiffness of the quantity of diaphragm formed thermoplastic composite components[J]. Thermoplastic Compos. Mater., 1990, 3(3): 23-29.

[6]  Delaloye S, Niedermeier M. Optimization of the diaphragm forming process for continuous fiber reinforced advanced thermoplastic composites[J]. Composites Mamfucruring, 1995, (6): 135-144.

[7]  Pantelakis Sp G, Katsiropoulos Ch V, Labeas G N, et al. A concept to optimize quality and cost in thermoplastic composite components applied to the production of helicopter canopies[J]. Composites: Part A, 2009, (40): 595-606.

[8]  McGuinness G B, Bradaigh C M O. Effect of perform shape on buckling of quasi isotropic thermoplastic composite laminates during sheet forming [J]. Composites Manufucturing, 1995, (6): 269-280.

[9]  Krebs J, Friedrich K, Bhattacharyya D. A direct comparison of matched die versus diaphragm forming[J]. Composites: Part A, 1998, (29A): 183-188.

[10]  Gutowski T G, Dillon G, Chey S, et al. Laminate wrinkling scaling laws for ideal composites[J]. Composites Manufacturing, 1995, (6): 123-134.

[11]  Pantelakis Sp G, Baxevani E A. Optimization of the diaphragm forming process with regard to product quality and cost[J]. Composites: Part A,2002, (33): 453-470.

[12]  苑世剑, 何祝斌, 刘钢. 轻合金热态液力成形技术[J]. 锻压技术, 2005, 30(6):75-80.

[13]  沈观林, 胡更开. 复合材料力学[M]. 北京:清华大学出版社, 2006.

[14]  杨乃宾. 新一代大型客机复合材料结构[J]. 航空学报, 2008, (3): 596-604.

[15]  陈亚莉. 高性能热塑性复合材料在飞机上的应用[J]. 航空维修与工程, 2003, (3): 28-30.

[16]  张兴金, 邓忠林. 浅谈纤维复合材料与中国大飞机[J]. 纤维复合材料, 2009, (2): 24-26.

[17]  段宝, 杨亚文, 王雅杰. 先进复合材料结构RTM技术现状及发展[J]. 沈阳航空工业学院学报, 2000, (3): 18-21.