[1] 陈帅, 李斌, 温金鹏, 等.软着陆气囊缓冲特性与参数设置的理论研究[J].振动与冲击, 2009, 28(4):25-28. doi: 10.3969/j.issn.1000-3835.2009.04.006

CHEN Shuai, LI Bin, WEN Jinpeng, et al. Cushioning characteristic and parameter design of a soft landing airbag[J]. Journal of Vibration and Shock, 2009, 28(4):25-28. doi: 10.3969/j.issn.1000-3835.2009.04.006
[2] 温金鹏, 李斌, 谭德伟, 等.考虑织布弹性的软着陆气囊缓冲特性研究[J].振动与冲击, 2010, 29(2):79-83. doi: 10.3969/j.issn.1000-3835.2010.02.018

WEN Jinpeng, LI Bin, TAN Dewei, et al. Cushioning characteristics of a soft landing airbag with elastic fabric[J]. Journal of Vibration and Shock, 2010, 29(2):79-83. doi: 10.3969/j.issn.1000-3835.2010.02.018
[3] 卫剑征, 谭惠丰, 万志敏, 等.缓冲气囊展开与缓冲着陆过程的仿真分析[J].航天返回与遥感, 2010, 31(5):1-8. doi: 10.3969/j.issn.1009-8518.2010.05.001

WEI Jianzheng, TAN Huifeng, WAN Zhimin, et al. Simulation for airbag deployment and landing process of inflatable landing vechiles[J]. Spacecraft Recovery & Remote Sensing, 2010, 31(5):1-8. doi: 10.3969/j.issn.1009-8518.2010.05.001
[4] 邓春燕, 裴锦华.全向式着陆缓冲气囊的折叠建模与充气过程仿真[J].南京航空航天大学学报, 2009, 41(增刊1):97-102. http://d.old.wanfangdata.com.cn/Periodical/njhkht2009z2022

DENG Chunyan, PEI Jinhua. Modeling and process simulating about folding and inflating of omni-directional-type airbag[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2009, 41(Suppl 1):97-102. http://d.old.wanfangdata.com.cn/Periodical/njhkht2009z2022
[5] 蔡文, 李斌, 温金鹏, 等.无人机软着陆气囊缓冲特性研究[J].兵工学报, 2014, 35(11):1867-1875. doi: 10.3969/j.issn.1000-1093.2014.11.019

CAI Wen, LI Bin, WEN Jinpeng, et al. Research on cushioning characteristics of UAV soft landing airbags[J]. Acta Armamentarii, 2014, 35(11):1867-1875. doi: 10.3969/j.issn.1000-1093.2014.11.019
[6] 邵志建, 裴锦华.某无人机横向圆柱排气式气囊着陆装置缓冲过程研究[J].航天返回与遥感, 2016, 37(2):26-33. http://d.old.wanfangdata.com.cn/Periodical/htfhyyg201602004

SHAO Zhijian, PEI Jinghua. Simulation of bi-cylindrical airbag cushioning system for pilotless aircraft[J]. Spacecraft Recovery & Remote Sensing, 2008, 20(5):1325-1327. http://d.old.wanfangdata.com.cn/Periodical/htfhyyg201602004
[7] 温金鹏, 李斌, 杨智春.缓冲气囊冲击减缓研究进展[J].宇航学报, 2010, 31(11):2438-2447. doi: 10.3873/j.issn.1000-1328.2010.11.002

WEN Jinpeng, LI Bin, YANG Zhichun. Progress of study on impact attenuation capability of airbag cushion system[J]. Journal of Astronautics, 2010, 31(11):2438-2447. doi: 10.3873/j.issn.1000-1328.2010.11.002
[8] 秦洪德, 赵林岳, 申静.入水冲击问题综述[J].哈尔滨工业大学学报, 2011(增刊1):152-157. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=QK201100301355

QIN Hongde, ZHAO Linyue, SHEN Jing. Review of water entry problem[J]. Journal of Harbin Institute of Technology, 2011(Suppl 1):152-157. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=QK201100301355
[9] WORTHINGTON A M, COLE R S. Impact with a liquid surface studied with aid of instantaneous photography[J]. Philosophical Transactions of the Royal Society of London, 1900, 194:175-199. doi: 10.1098/rsta.1900.0016
[10] 王永虎, 石秀华.入水冲击问题研究的现状与进展[J].爆炸与冲击, 2008, 28(3):276-282. doi: 10.3321/j.issn:1001-1455.2008.03.014

WANG Yonghu, SHI Xiuhua. Review on research and development of water-entry impact problem[J]. Explosion and Shock Waves, 2008, 28(3):276-282. doi: 10.3321/j.issn:1001-1455.2008.03.014
[11] 卢炽华, 何友声.二维弹性结构入水冲击过程中的流固耦合效应[J].力学学报, 2000, 32(2):129-140. doi: 10.3321/j.issn:0459-1879.2000.02.001

LU Chihua, HE Yousheng. Coupled analysis of nonlinear interaction between fluid and structure during impact[J]. Acta Mechanica Sinica, 2000, 32(2):129-140. doi: 10.3321/j.issn:0459-1879.2000.02.001
[12] 李飞, 孙凌玉, 张广越, 等.圆柱壳结构入水过程的流固耦合仿真与试验[J].北京航空航天大学学报, 2007, 33(9):1117-1120. doi: 10.3969/j.issn.1001-5965.2007.09.027

LI Fei, SUN Lingyu, ZHANG Guangyue, et al. Simulation and experiment of cylinder shell structure dropping into water based on fluid structure interaction[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(9):1117-1120. doi: 10.3969/j.issn.1001-5965.2007.09.027
[13] 施红辉, 胡青青, 陈波, 等.钝体倾斜和垂直冲击入水时引起的超空泡流动特性实验研究[J].爆炸与冲击, 2015, 35(5):617-624. http://www.bzycj.cn/CN/abstract/abstract9509.shtml

SHI Honghui, HU Qingqing, CHEN Bo, et al. Experimental study of supercavitating flows induced by oblique and vertical water entry of blunt bodies[J]. Explosion and Shock Waves, 2015, 35(5):617-624. http://www.bzycj.cn/CN/abstract/abstract9509.shtml
[14] 程涵.气囊工作过程仿真研究[D].南京: 南京航空航天大学, 2009. http://cdmd.cnki.com.cn/Article/CDMD-10287-1011253523.htm

CHENG Han. Numerical simulation research on airbag working process[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009. http://cdmd.cnki.com.cn/Article/CDMD-10287-1011253523.htm
[15] 李裕春, 时党勇, 赵远.ANSYS 11.0/LS-DYNA基础理论与工程实践[M].北京:中国水利水电出版社, 2008.
[16] 蒋克强, 张遵鸥, 张培成.基于ANSYS/LS-DYNA的示位标入水冲击仿真分析[J].电子机械工程, 2012, 28(2):15-17, 21. doi: 10.3969/j.issn.1008-5300.2012.02.005

JIANG Keqiang, ZHANG Zun'ou, ZHANG Peicheng. Water-entry impact simulation analysis of a position indicating radio beacon based on ANSYS/LS-DYNA[J]. Electro-Mechanical Engineering, 2012, 28(2):15-17, 21. doi: 10.3969/j.issn.1008-5300.2012.02.005
[17] 刘树红, 吴玉林, 左志钢.应用流体力学[M].北京:清华大学出版社, 2012.
[18] 郭子涛, 张伟, 郭钊, 等.截卵形弹水平入水的速度衰减及空泡扩展特性[J].爆炸与冲击, 2017, 37(4):727-733. http://www.bzycj.cn/CN/abstract/abstract9775.shtml

GUO Zitao, ZHANG Wei, GUO Zhao, et al. Characteristics of velocity attenuation and cavity expansion induced by horizontal water-entry of truncated-ogive nosed projectiles[J]. Explosion and Shock Waves, 2017, 37(4):727-733. http://www.bzycj.cn/CN/abstract/abstract9775.shtml
[19] 何春涛, 王聪, 魏英杰, 等.圆柱体垂直入水空泡形态试验[J].北京航空航天大学学报, 2012, 38(11):1542-1546. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=QK201205748643

HE Chuntao, WANG Cong, WEI Yingjie, et al. Vertical water entry cavity of cylinder body[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(11):1542-1546. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=QK201205748643
[20] 邓春燕, 裴锦华.全向式气囊着陆装置缓冲过程的仿真研究[J].中国空间科学技术, 2010, 30(1):78-83. http://d.old.wanfangdata.com.cn/Periodical/zgkjkxjs201001012

DENG Chunyan, PEI Jinhua. Simulation about buffer process of omni-directional-type airbag landing device[J]. Chinese Space Science and Technology, 2010, 30(1):78-83. http://d.old.wanfangdata.com.cn/Periodical/zgkjkxjs201001012
[21] 李名琦.应急气囊着水冲击特性的试验研究与数值分析[D].南京: 南京航空航天大学, 2008. doi: 10.7666/d.d053189
[22] 戴华杰, 胡振东, 咸奎成, 等.火星探测器气囊缓冲系统着陆过程仿真[J].力学季刊, 2010, 31(4):555-561. http://d.old.wanfangdata.com.cn/Periodical/lxjk201004014

DAI Huajie, HU Zhendong, XIAN Kuicheng, et al. Simulation analysis for landing process of a Mars detector with airbag buffer system[J]. Chinese Quarterly of Mechanics, 2010, 31(4):555-561. http://d.old.wanfangdata.com.cn/Periodical/lxjk201004014