Page 105 - 《爆炸与冲击》2026年第3期

第 46 卷 张柱国，等： 泡沫铝夹芯结构抗鸟体冲击吸能机理及在飞机机头端框挡板中的应用 第 3 期

impact [J]. Explosion and Shock Waves, 2018, 38(2): 373–380. DOI: 10.11883/bzycj-2016-0232.
[25] MCCARTHY M A, XIAO J R, PETRINIC N, et al. Modelling of bird strike on an aircraft wing leading edge made from fibre
metal laminates. Part 1: material modelling [J]. Applied Composite Materials, 2004, 11(5): 295–315. DOI: 10.1023/B:ACMA.
0000037133.64496.13.
[26] LIU J, LI Y L, YU X C, et al. A novel design for reinforcing the aircraft tail leading edge structure against bird strike [J].
International Journal of Impact Engineering, 2017, 105: 89–101. DOI: 10.1016/j.ijimpeng.2016.12.017.
[27] ZHENG Z J, YU J L, WANG C F, et al. Dynamic crushing of cellular materials: a unified framework of plastic shock wave
models [J]. International Journal of Impact Engineering, 2013, 53: 29–43. DOI: 10.1016/j.ijimpeng.2012.06.012.
[28] ZHANG Y, HE S Y, LIU J G, et al. Density gradient tailoring of aluminum foam-filled tube [J]. Composite Structures, 2019,
220: 451–459. DOI: 10.1016/j.compstruct.2019.04.026.
[29] 牛卫晶. 冲击载荷下泡沫铝夹芯防护结构的侵彻动力学行为研究 [D]. 太原: 太原理工大学, 2015. DOI: 10.7666/d.
Y2798431.
NIU W J. Research on the penetration behavior of sandwich protective structures with aluminum foam cores under impact
loading [D]. Taiyuan: Taiyuan University of Technology, 2015. DOI: 10.7666/d.Y2798431.
[30] 黄苏南, 丁圆圆, 王士龙, 等. 闭孔泡沫铝动态材料参数的实验研究 [J]. 实验力学, 2018, 33(6): 851–861. DOI: 10.7520/
1001-4888-17-211.
HUANG S N, DING Y Y, WANG S L, et al. Experimental investigation on dynamic material parameters of closed-cell
aluminium foam [J]. Journal of Experimental Mechanics, 2018, 33(6): 851–861. DOI: 10.7520/1001-4888-17-211.
[31] 吕怡楠. 梯度泡沫铝的结构调控及冲击性能研究 [D]. 南京: 东南大学, 2020. DOI: 10.27014/d.cnki.gdnau.2020.000987.
LV Y N. Gradient regulation and impact properties of density-graded aluminum foam [D]. Nanjing: Southeast University,
2020. DOI: 10.27014/d.cnki.gdnau.2020.000987.
[32] BUDGEY R. The development of a substitute artificial bird by the international bird strike research group for use in aircraft
component testing [C]//Proceedings of International Bird Strike Committee 25. Amsterdam, 2000: 17–21.
[33] 刘军, 李玉龙, 刘元镛. 基于 SPH 方法的叶片鸟撞数值模拟研究 [J]. 振动与冲击, 2008, 27(9): 90–93, 185. DOI: 10.13465/
j.cnki.jvs.2008.09.019.
LIU J, LI Y L, LIU Y Y. Numerical simulation study of bird-impact on a blade using SPH method [J]. Journal of Vibration
and Shock, 2008, 27(9): 90–93, 185. DOI: 10.13465/j.cnki.jvs.2008.09.019.
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