[1] 蒋浩征, 周兰庭, 蔡汉文. 火箭战斗部设计原理[M]. 北京: 国防工业出版社, 1982.
[2] BALL R E. The fundamentals of aircraft combat survivability analysis and design [M]. 2nd ed. Reston: American Institute of Aeronautics and Astronautics Inc., 2003.
[3] 刘彤. 防空战斗部杀伤威力评估方法研究[D]. 北京: 北京理工大学, 2004.
[4] 裴扬, 宋笔锋, 石帅. 飞机作战生存力分析方法研究进展与挑战 [J]. 航空学报, 2016, 37(1): 216–234.

PEI Y, SONG B F, SHI S. Analysis method of aircraft combat survivability: progress and challenge [J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(1): 216–234.
[5] 司凯, 李向东, 郭超, 等. 破片式战斗部对飞机类目标毁伤评估方法研究 [J]. 弹道学报, 2017, 29(4): 52–57. doi: 10.3969/j.issn.1004-499X.2017.04.009

SI K, LI X D, GUO C, et al. Research on damage assessment method of fragmentation warhead against airplane targets [J]. Journal of Ballistics, 2017, 29(4): 52–57. doi: 10.3969/j.issn.1004-499X.2017.04.009
[6] 梁斌, 冯高鹏, 周婕群, 等. 离散杆和EFP组合战斗部对飞机毁伤效应研究 [J]. 弹箭与制导学报, 2017, 37(1): 39–45.

L1ANG B, FENG G P, ZHOU J Q, et al. Research on the damage effect of EFP combined warhead and discrete rod to battleplane [J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2017, 37(1): 39–45.
[7] KONOKMAN H E, KAY A M. Analysis of aircraft survivability against fragmenting warhead threat: AIAA-2014.0355 [R]. Reston: AIAA, 2014.
[8] 黄季墀, 汪海. 飞机结构设计与强度计算[M]. 上海: 上海交通大学出版社, 2012.
[9] 陶梅贞. 现代飞机结构综合设计[M]. 西安: 西北工业大学出版社, 2014.
[10] 张森林. 在核爆炸冲击波环境中飞行飞机的结构动力响应分析 [J]. 航空学报, 1992, 13(9): A510–A515.

ZHANG S L. Analysis of structural dynamic response for aircraft to petrating in the environment of nuclear explosion shock waves [J]. Acta Aeronautica et Astronautica Sinica, 1992, 13(9): A510–A515.
[11] 刘杨, 陆浦. 一种机翼弯剪载荷包线近似计算方法 [J]. 航空工程进展, 2013, 4(2): 241–246. doi: 10.3969/j.issn.1674-8190.2013.02.018

LIU Y, LU P. Approximation method for calculating the wing load envelope of bending moment and shear force [J]. Advances in Aeronautical Science and Engineering, 2013, 4(2): 241–246. doi: 10.3969/j.issn.1674-8190.2013.02.018
[12] 隋树元, 王树山. 终点效应学[M]. 北京: 国防工业出版社, 2000.