[1]中国民用航空总局. CCAR-25-R2 中国民用航空规章第25部[S]. 北京: 中国民用航空总局, 2001.
Civil Aviation Administration of China. CCAR-25-R2 China civil aviation rules: Vol. 25[S]. Beijing: Civil Aviation Administration of China, 2001. (in Chinese)
[2]罗漳平, 向锦武. 直升机起落架抗坠毁性能的有限元仿真评估[J]. 航空学报, 2003, 24(3): 216-219.
Luo Zhangping, Xiang Jinwu. Crashworthiness performance evaluation to helicopter landing gear by finite element simulation[J]. Acta Aeronautica et Astronautica Sinica, 2003, 24(3): 216-219. (in Chinese)
[3]杨嘉陵, 吴卫华, 赵岩, 等. 跪式起落架在武装直升机坠毁过程中能量吸收能力研究(I)——数值仿真计算[J]. 航空学报, 2002, 23 (1): 23-27.
Yang Jialing, Wu Weihua, Zhao Yan, et al. Energy absorbing capability of kneeling landing gear for new type armed helicopters during crash process (I): numerical simulation [J]. Acta Aeronautica et Astronautica Sinica, 2002, 23(1): 23-27. (in Chinese)
[4]杨嘉陵, 吴为华, 赵岩, 等. 跪式起落架在武装直升机坠毁过程中能量吸收能力研究(II)——理论模型分析[J]. 航空学报, 2002, 23(1): 28-32.
Yang Jialing, Wu Weihua, Zhao Yan, et al. Energy absorbing capability of kneeling landing gear for new type armed helicopters during crash process(II): theoretical model analysis[J]. Acta Aeronautica et Astronautica Sinica, 2002, 23(1): 28-32. (in Chinese)
[5]倪先平, 王永亮, 荚淑萍, 等. 直升机机身下部复合材料典型结构耐坠特性研究[J]. 复合材料学报, 2003, 20(4): 51-57.
Ni Xianping, Wang Yongliang, Jia Shuping, et al. Analysis of crash impact behaviour of typical composite components of helicopter bottom structure[J]. Acta Materiea Compositae Sinica, 2003, 20(4): 51-57. (in Chinese)
[6]Thomson R G, Caiafa C. Designing of aircraft structural crashworthiness[J]. Journal of Aircraft, 1982, 19(10): 868-874.
[7]Cronkhite J D, Berry V L. Crashworthy airframe design concepts fabrication and testing[R]. NASA Contractor Report 3603, 1982.
[8]Wiggenraad J F M, Michielsen A L P J, Santoro D, et al. Development of a crashworthy composite fuselage structure for a commuter aircraft[R]. NLR, NLR-TP-99532, 1999.
[9]Jackson K E, Fasanella E L, Kellas S. Development of a scale model composite fuselage concept for improved crashworthiness[J]. Journal of Aircraft, 2001, 38(1): 95-103.
[10]Meng F X, Zhou Q, Yang J L. Improvement of crashworthiness behaviour for simplified structural models of aircraft fuselage[J]. International Journal of Crashworthiness, 2009, 14(1): 1-15.
[11]Bark L W, Yaniv G. Cost-effective production of helicopter energy-absorbing subfloor structures with advanced thermoplastic composites[C]∥the American Helicopter Society 49th Annual Forum. 1993: 519-529.
[12]刘瑞同, 王鑫伟, 荚淑萍. 碳纤维-环氧树脂波纹梁吸能能力的试验研究[J]. 航空学报, 2001, 22(1): 59-61.
Liu Ruitong, Wang Xinwei, Jia Shuping. Experimental study on energy absorption of carbon-epoxy waved beams[J]. Acta Aeronautica et Astronautica Sinica, 2001, 22(1): 59-61. (in Chinese)
[13]龚俊杰, 王鑫伟. 复合材料波纹梁吸能能力的数值模拟[J]. 航空学报, 2008, 26(3): 298-302.
Gong Junjie, Wang Xinwei. Numerical simulation of energy absorption capability of composite waved beams[J]. Acta Aeronautica et Astronautica Sinica, 2008, 26(3): 298-302. (in Chinese)
[14]Bisagni C, Lanzi L, Ricci S. Size and topological optimization for crashworthiness design of helicopter subfloor[R]. AIAA-2002-5484, 2002.
[15]Hallquist J O. LS-DYNA theoretical manual[M]. California: Livermore Software Technology Corporation, 1998: 77-88.
[16]何欢. 通用飞机结构耐撞性分析与设计关键技术研究[D]. 南京:南京航空航天大学航空宇航学院, 2007.
He Huan. Key technology of general aircraft crash simulation and crashworthiness design[D]. Nanjing: College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, 2007. (in Chinese) |