飞机撞击建(构)筑物研究进展

刘晶波; 韩鹏飞; 林丽; 陆新征; 岑松

doi:10.11883/1001-1455(2016)02-0269-10

飞机撞击建(构)筑物研究进展

doi: 10.11883/1001-1455(2016)02-0269-10

刘晶波¹,
韩鹏飞^{1, 2, ,},
林丽³,
陆新征¹,
岑松³

1.
清华大学土木水利学院土木工程系, 北京 100084
2.
总参谋部工程兵科研三所, 河南洛阳 471023
3.
清华大学航天航空学院工程力学系, 北京 100084

基金项目:

国家科技重大专项项目 2011ZX06002-10

详细信息

作者简介:
刘晶波(1956—)，男，博士，教授，博士生导师

通讯作者:
韩鹏飞，feixuehan2003@sina.com

中图分类号: O383; TU312; TB122
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- 被引次数: 0
出版历程
- 收稿日期: 2014-09-15
- 修回日期: 2014-11-25
- 刊出日期: 2016-03-25

Research progress of buildings and structures subjected to aircraft impact

Liu Jingbo¹,
Han Pengfei^{1, 2
, ,},
Lin Li³,
Lu Xinzheng¹,
Cen Song³

1.
Department of Civil Engineering, School of Civil Engineering, Tsinghua University, Beijing 100084, China
2.
The Third Research Institute of Engineering Corps, General Staff of PLA, Luoyang 471023, Henan, China
3.
Department of Engineering Mechanics, School of Aerospace, Tsinghua University, Beijing 100084, China

摘要

摘要: 飞机撞击重要建(构)筑物会导致灾难性后果。本文从试验研究、理论分析、数值模拟等3个方面对飞机撞击建(构)筑物的国内外研究现状，相关研究难点、需要注意的问题和研究方向及趋势进行总结，包括：缩比试验的系统和验证，飞机撞击力模型，撞击所致局部破坏计算公式，飞机和建(构)筑物的精细化建模，撞击所致振动特性，撞击荷载和火荷载对结构的耦合毁伤效应，一般模型和精细化模型、解耦和耦合方法以及不同数值模拟程序计算结果的对比分析等方面，以期为后续研究提供参考。
- 爆炸力学 /
- 精细化模型 /
- 撞击载荷 /
- 耦合毁伤效应 /
- 飞机撞击
Abstract: Studies on buildings and structures subjected to aircraft impact have been of greater concern, because malicious aircraft crash is one of the major means adopted in terrorist attacks due to the disastrous consequences and extremely bad influences involved. As the aircraft impact is related with multiple scientific issues, in this paper, the latest developments in the study of buildings and structures subjected to aircraft impact at home and aboard are summarized from three respects covered by test study, theoretical analysis, and numerical simulation, with special focus on difficulties and problems in research as well as the future research direction and trend, including firstly the system research and validation for scale model test, secondly the impact force model and local damage calculation formulas research, thirdly the establishment of the refined model of aircraft, buildings and structures, fourthly the vibration characteristics of buildings and structures subjected to aircraft impact, fifthly the coupling damage effect of impact load and fire load, and finally the comparative analysis of results calculated by the general model and the refined model, decoupling and coupling method, and various numerical simulation programs.
- mechanics of explosion /
- refined model /
- impact load /
- coupling damage effect /
- aircraft impact

HTML全文

图 1 撞击试验中弹体示意图

Figure 1. Sketch of projectile in impact test

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图 2 装有液体的弹体撞击试验装置

Figure 2. Impact test apparatus of projectile loaded with liquid

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图 3 双钢板混凝土复合靶板结构图

Figure 3. Structural diagram of steel-concrete-steel sandwich composite plate target

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图 4 加速系统和弹体

Figure 4. Acceleration system and projectile

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图 5 F-4鬼怪飞机撞击和靶板破坏情景^[17]

Figure 5. View of F-4 phantom aircraft during impact and target damage after impact^[17]

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图 6 机撞击变形靶板(集中质量模型)

Figure 6. Aircraft impact on deformable target(lumped-mass model)

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图 7 F-16战机撞击双钢板混凝土板

Figure 7. F-16 Aircraft impact on steel-concrete-steel sandwich composite plate

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8(a) 波音767飞机撞击世贸大厦实际场景

8(a). Actual photograph of Boeing 767 aircraft impacting the World Trade Center

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8(b) 波音767飞机撞击世贸大厦数值模拟结果

8(b). Simulation result of Boeing 767 aircraft impacting the World Trade Center

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表 1 文献中撞击力计算公式

Table 1. Impact force calculation formulas in reference

模型来源	撞击力计算公式
文献[1]	F=p_c+μv_r²
文献[20]	$ F=-\left[\frac{1}{2} \mu v_{\mathrm{r}}^{2}(1+f)+e\right]$
文献[21]	F=p_c+αμv_r²
文献[22]	$ F=p_{\mathrm{c}}+\frac{1}{2} \mu v_{\mathrm{r}}^{2}(1+f)+\sqrt{f} m_{\mathrm{c}} \frac{\mathrm{d} v_{\mathrm{t}}}{\mathrm{d} t}+\frac{1}{v_{\mathrm{r}}} \frac{\mathrm{d} E_{\mathrm{a}}}{\mathrm{d} t}$

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