[1] 杜善义. 先进复合材料和航空航天. 复合材料学报, 2007, 24(1): 1-12.
[2] 陈绍杰. 复合材料技术与大飞机. 航空学报, 2008, 29(3): 605-610.
[3] Li Y G, Li N, James G. Tooling design and microwave curing technologies for the manufacturing of fiber-reinforced polymer composites in aerospace applications. The International Journal of Advanced Manufacturing Technology. 2014, 70(1-4): 591-606.
[4] Li N, Li Y G, James G. Analysis and optimization of temperature distribution in carbon fiber reinforced composite materials during microwave curing process. Journal of Materials Processing Technology, 2014, 214(3): 544-550.
[5] Lin Y, Ye L, Zhong Q S, Guang Meng. Functionalized composite structures for new generation airframes:a review. Composites Science and Technology, 2005(65): 1436-1446.
[6] 邢丽英, 蒋诗才, 周正刚. 先进树脂基复合材料制造技术进展. 复合材料学报, 2013 (2): 1-9.
[7] Lee W L, Springer G S. Microwave curing of composite materials. Journal of Composite Materials. 1984, 18 (4): 387-409.
[8] Boey F Y, Yap B H. Microwave curing of an epoxy-amine system: effect of curing agent on the glass-transition temperature. Polymer Testing, 2001(20): 837-845.
[9] 刘学清, 王源升. 微波固化环氧树脂(E44/DDM)的热性能及膨胀性能. 高分子材料科学与工程, 2004 (3): 111-113.
[10] Wei J, Hawley M C, Delong J D, et al. Comparison of microwave and thermal cure of epoxy resins. Polymer Engineering & Science, 1993 (33): 1132-1140.
[11] 高树理. 微波功能复合材料的应用与发展. 航空制造技术, 2004(7): 49-59.
[12] 谷晓昱, 张军营. 微波固化环氧树脂中非热效应的研究. 高分子材料科学与工程, 2006(22): 183-186.
[13] 黎炎图, 王超英, 杜作娟, 等. 短切碳纤维电磁散射特性仿真研究.计算机仿真, 2011(28): 139-143.
[14] 程群峰, 方征平,益小苏, 等. 双马来酰亚胺树脂体系的固化动力学和TTT图. 材料工程, 2008 (S1): 188-192.
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