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长杆高速侵彻问题研究进展 被引量:22
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作者 焦文俊 陈小伟 《力学进展》 EI CSCD 北大核心 2019年第1期312-391,共80页
由高密度金属制成的长杆弹在1.5~3.0 km/s的高速下具有很强的侵彻和贯穿能力,长杆高速侵彻问题现已成为穿甲侵彻领域的研究热点.本文综述了长杆高速侵彻问题的最新研究进展,首先介绍了长杆高速侵彻的基本概念、研究方法和理论模型;其... 由高密度金属制成的长杆弹在1.5~3.0 km/s的高速下具有很强的侵彻和贯穿能力,长杆高速侵彻问题现已成为穿甲侵彻领域的研究热点.本文综述了长杆高速侵彻问题的最新研究进展,首先介绍了长杆高速侵彻的基本概念、研究方法和理论模型;其次重点论述了研究中关注的突出问题与应用,包括弹靶材料性质、长杆弹头部形状、长径比效应与分段杆设计、陶瓷靶抵抗长杆侵彻与界面击溃和非理想长杆侵彻;最后对未来的研究工作提出一些建议. 展开更多
关键词 长杆弹 高速 侵彻 理论模型 穿甲力学
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From concept to reality-A review to the primary test stand and its preliminary application in high energy density physics 被引量:21
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作者 Jianjun Deng Weiping Xie +28 位作者 Shuping Feng Meng Wang Hongtao Li Shengyi Song Minghe Xia Ji Ce An He Qing Tian Yuanchao Gu Yongchao Guan Bin Wei Xianbin Huang Xiaodong Ren Jiakun Dan Jing Li Shaotong Zhou Hongchun Cai Siqun Zhang Kunlun Wang Qiang Xu Yujuan Wang Zhaohui Zhang Guilin Wang Shuai Guo Yi He Yiwei Zhou Zhanji Zhang Libing Yang Wenkang Zou 《Matter and Radiation at Extremes》 SCIE EI CAS 2016年第1期48-58,共11页
Pulsed power technology,whereas the electrical energy stored in a relative long period is released in much shorter timescale,is an efficient method to create high energy density physics(HEDP)conditions in laboratory.A... Pulsed power technology,whereas the electrical energy stored in a relative long period is released in much shorter timescale,is an efficient method to create high energy density physics(HEDP)conditions in laboratory.Around the beginning of this century,China Academy of Engineering Physics(CAEP)began to build some experimental facilities for HEDP investigations,among which the Primary Test Stand(PTS),a multi-module pulsed power facility with a nominal current of 10 MA and a current rising time~90 ns,is an important achievement on the roadmap of the electro-magnetically driven inertial confinement fusion(ICF)researches.PTS is the first pulsed power facility beyond 10 TW in China.Therefore,all the technologies have to be demonstrated,and all the engineering issues have to be overcome.In this article,the research outline,key technologies and the preliminary HEDP experiments are reviewed.Prospects on HEDP research on PTS and pulsed power development for the next step are also discussed. 展开更多
关键词 High energy density physics Inertial confinement fusion Z-PINCH Isentropic compression hypervelocity flyer launch Pulsed power Primary Test Stand
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Preliminary Study on Diagnostic Techniques for Transient Plasma Generated by Hypervelocity Impact 被引量:16
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作者 唐恩凌 张庆明 +1 位作者 何远航 张健 《Plasma Science and Technology》 SCIE EI CAS CSCD 2008年第6期735-738,共4页
A fast-sweep Langmuir probe (FSLP) diagnostic system was designed and applied to obtain the electron temperature fluctuations of a transient plasma. The diagnostic system consists of a single Langmuir probe driven b... A fast-sweep Langmuir probe (FSLP) diagnostic system was designed and applied to obtain the electron temperature fluctuations of a transient plasma. The diagnostic system consists of a single Langmuir probe driven by a high frequency sinusoidal voltage. The current-voltage I- V characteristics can be recorded by sweeping the voltage and measuring the current with an appropriate circuit. This new instrument is based on a dual channel circuit that compensates for stray capacitance. The current and voltage spectra were acquired from the probe synchronously by a digital oscilloscope. The aim of this work was to apply the FSLP diagnostic system to a time- dependent plasma generated by a hypervelocity impact between the LY12 Aluminum projectile and LY12 Aluminum target. 展开更多
关键词 hypervelocity impact fast-sweep Langmuir probe electron temperature
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Preliminary Study on Magnetic Induction Intensity Induced by Plasma During Hypervelocity Impact 被引量:13
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作者 Tang Enling Zhang Qingming Zhang Jian 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2009年第4期387-392,共6页
An experimental system has been built to produce and measure the magnetic field in the backward ejected matter during hypervelocity impact. The designs of measurement system and coil, the choice of associated equipmen... An experimental system has been built to produce and measure the magnetic field in the backward ejected matter during hypervelocity impact. The designs of measurement system and coil, the choice of associated equipment, and the system calibration are also described in detail. The measurement of magnetic induction intensity for different given coil positions and azimuth angles are performed with two-stage light-gas gun. On condition that impact velocities are approximately equal and incidence angles are 45°, 60° and 90° respectively, the relationship between average magnetic induction intensity and impact angle at different time spans is obtained. Experimental results show that the average magnetic induction intensity with incidence angle of 90° is larger than those with incidence angles of 45°and 60°. 展开更多
关键词 hypervelocity impact PLASMA magnetic fields measurement system magnetic induction intensity
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激光驱动飞片实验研究及其应用分析 被引量:12
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作者 谷卓伟 孙承纬 罗利军 《红外与激光工程》 EI CSCD 北大核心 2002年第5期428-431,共4页
利用小型固体激光器在 10 0~ 30 0mJ能量范围内成功驱动了 5 .5 μm厚度铝飞片 ,最高速度达到 6 .6km s ,实验得到飞片速度与能量密度的关系。详细介绍了实验装置、测试系统和实验方法 ,并对实验测试系统进行了分析。对回收样品的分析... 利用小型固体激光器在 10 0~ 30 0mJ能量范围内成功驱动了 5 .5 μm厚度铝飞片 ,最高速度达到 6 .6km s ,实验得到飞片速度与能量密度的关系。详细介绍了实验装置、测试系统和实验方法 ,并对实验测试系统进行了分析。对回收样品的分析表明 :飞片具有较好的平面性、完整性和重复性。对激光驱动飞片技术在模拟太空高速微粒的应用可能性进行了分析 ,目前的研究表明 :激光驱动飞片技术可以成为一种模拟太空高速粒子的有效实验手段。 展开更多
关键词 飞片 实验 脉冲激光 驱动 太空微粒 高速 固体激光器
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电磁轨道发射器刨削产生特征与研究现状 被引量:12
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作者 雷彬 朱仁贵 +3 位作者 张倩 李鹤 李治源 纪斌义 《兵器材料科学与工程》 CAS CSCD 2011年第3期76-81,共6页
超高速刨削是超高速滑动下轨道表面的一种损伤形式。刨削的出现降低系统发射效率、缩短轨道寿命,增大射弹方向误差。从刨削产生规律、刨槽形貌特性和发生发展物理机制3个方面,较全面的总结轨道上超高速刨削损伤的研究现状。结合轨道炮... 超高速刨削是超高速滑动下轨道表面的一种损伤形式。刨削的出现降低系统发射效率、缩短轨道寿命,增大射弹方向误差。从刨削产生规律、刨槽形貌特性和发生发展物理机制3个方面,较全面的总结轨道上超高速刨削损伤的研究现状。结合轨道炮特有的超高速大电流特性,展望轨道炮抑制刨削的研究趋势。 展开更多
关键词 超高速 饱削 轨道炮
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超高速模型及其等离子体鞘套RCS特性研究(英文) 被引量:13
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作者 曾学军 于哲峰 +4 位作者 部绍清 柳森 马平 石安华 梁世昌 《空气动力学学报》 EI CSCD 北大核心 2010年第6期645-649,共5页
为了研究等离子体对超高速模型雷达散射截面的影响,利用气动物理靶测量超高速模型及其绕流的雷达散射截面(RCS),给出了雷达接收信号、信号频谱和模型雷达散射截面的一维距离像。利用时域有限差分方法(FDTD)分析了等离子体鞘套对模型电... 为了研究等离子体对超高速模型雷达散射截面的影响,利用气动物理靶测量超高速模型及其绕流的雷达散射截面(RCS),给出了雷达接收信号、信号频谱和模型雷达散射截面的一维距离像。利用时域有限差分方法(FDTD)分析了等离子体鞘套对模型电磁散射特性的影响。将数值模拟结果和试验结果进行了对比,对比结果显示二者符合得很好。数值模拟结果还表明雷达入射角小角度偏移对测量结果有较大影响。 展开更多
关键词 再入 雷达散射面积 等离子体 超高速
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二级轻气炮模拟空间碎片超高速碰撞试验技术 被引量:12
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作者 杨继运 《航天器环境工程》 2006年第1期16-22,共7页
二级轻气炮是用来模拟空间碎片超高速碰撞效应的重要设备。文章首先介绍了目前二级轻气炮国内外的发展的概况;阐述了其工作原理及所使用的工作气体和试验用品;然后讨论了影响二级轻气炮性能的初始注气压力、活塞速度、弹丸释放压力、活... 二级轻气炮是用来模拟空间碎片超高速碰撞效应的重要设备。文章首先介绍了目前二级轻气炮国内外的发展的概况;阐述了其工作原理及所使用的工作气体和试验用品;然后讨论了影响二级轻气炮性能的初始注气压力、活塞速度、弹丸释放压力、活塞质量、弹丸质量等若干参量;最后对反映二级轻气炮性能的重要指标弹丸出口速度和动态碰撞角的测试技术和方法进行了分析。 展开更多
关键词 二级轻气炮 模拟 空间碎片 超高速碰撞 试验技术 hypervelocity Impact 弹丸质量 注气压力 重要设备 性能 碰撞效应 活塞 工作原理 工作气体 出口速度 测试技术 试验用 碰撞角 指标 国内
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电磁轨道炮外弹道建模与仿真研究 被引量:11
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作者 谢杨柳 马萍 杨明 《计算机仿真》 CSCD 北大核心 2009年第2期45-49,共5页
针对电磁轨道炮在发射时存在初始扰动,飞行时由于速度极大引起气动烧蚀改变气动外形,因此有必要建立电磁轨道炮外弹道数学模型,分析其外弹道特性。通过分析了电磁轨道炮外弹道建模方法,建立了电磁轨道炮的外弹道数学模型。根据不同技战... 针对电磁轨道炮在发射时存在初始扰动,飞行时由于速度极大引起气动烧蚀改变气动外形,因此有必要建立电磁轨道炮外弹道数学模型,分析其外弹道特性。通过分析了电磁轨道炮外弹道建模方法,建立了电磁轨道炮的外弹道数学模型。根据不同技战术指标建立初始随机概率模型,用MonteCarlo方法对电磁轨道炮的外弹道特性进行仿真。仿真结果给出了一定散布范围内的高低概率误差和方向概率误差,对电磁轨道炮武器系统设计指标的提出有参考价值。 展开更多
关键词 轨道炮 外弹道 超高速 弹丸 仿真
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超高速动能反坦克导弹技术 被引量:10
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作者 高原 谷良贤 《火力与指挥控制》 CSCD 北大核心 2008年第10期1-4,共4页
随着未来主战坦克防御能力的极大提高,常规反装甲武器已远远不能适应现代战争的需求。动能穿甲作为一种新概念的反装甲技术,能够有效地杀伤普通反坦克导弹束手无策的复合装甲和主动防护系统。介绍了超高速动能反坦克导弹的基本原理、结... 随着未来主战坦克防御能力的极大提高,常规反装甲武器已远远不能适应现代战争的需求。动能穿甲作为一种新概念的反装甲技术,能够有效地杀伤普通反坦克导弹束手无策的复合装甲和主动防护系统。介绍了超高速动能反坦克导弹的基本原理、结构组成以及国外发展状况,分析了超高速动能反坦克导弹的关键技术,并指出了其发展趋势。 展开更多
关键词 超高速 动能穿甲 反坦克导弹 关键技术
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Modeling on the shock wave in spheres hypervelocity impact on flat plates 被引量:9
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作者 Ken Wen Xiao-Wei Chen De-Ning Di 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2019年第4期457-466,共10页
In hypervelocity impacts of projectiles into thin flat targets,shock initiation and interaction dominate the responses of projectiles and targets,and especially dominate the features of the debris cloud.To estimate th... In hypervelocity impacts of projectiles into thin flat targets,shock initiation and interaction dominate the responses of projectiles and targets,and especially dominate the features of the debris cloud.To estimate the geometric features of the wave front during the first complete propagation in the sphericalprojectile,the Geometric Propagation Model(GPM)is built in this paper to describe the geometry of the shock wave front,which proposes an ellipse contour as a function of time and equivalent speed.The GPM identifies the geometric features of the wave front as a function of time and impact velocity successfully.Combined with the GPM and SPH simulation,the shock pressure distribution and attenuation in the spherical-projectile have been obtained.Meanwhile,the attenuation of shock pressure and speed are presented as a function of impact velocity,respectively,and a method for obtaining the equivalent speed of the shock wave is proposed by the GPM.The GPM may be applicable to hypervelocity events involving any monolithic materials as long as the equivalent speed could be supplied from numerical simulation.The GPM proposed in this paper and the corresponding shock wave analysis provide a new insight into the processes of the quantitative analysis of the initiation of the debris cloud. 展开更多
关键词 hypervelocity impact Shock wave NUMERICAL simulation DEBRIS CLOUD formation
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Fragment Identification and Statistics Method of Hypervelocity Impact SPH Simulation 被引量:8
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作者 ZHANG Xiaotian JIA Guanghui HUANG Hai 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2011年第1期18-24,共7页
A comprehensive treatment to the fragment identification and statistics for the smoothed particle hydrodynamics (SPH) simulation of hypervelocity impact is presented. Based on SPH method, combined with finite elemen... A comprehensive treatment to the fragment identification and statistics for the smoothed particle hydrodynamics (SPH) simulation of hypervelocity impact is presented. Based on SPH method, combined with finite element method (FEM), the computation is performed. The fragments are identified by a new pre- and post-processing algorithm and then converted into a binary graph. The number of fragments and the attached SPH particles are determined by counting the quantity of connected domains on the binary graph. The size, velocity vector and mass of each fragment are calculated by the particles’ summation and weighted average. The dependence of this method on finite element edge length and simulation terminal time is discussed. An example of tungsten rods impacting steel plates is given for calibration. The computation results match experiments well and demonstrate the effectiveness of this method. 展开更多
关键词 IMPACT SIMULATION smoothed particle hydrodynamics FRAGMENT hypervelocity
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Effect of compressibility on the hypervelocity penetration 被引量:6
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作者 W.J.Song X.W.Chen P.Chen 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2018年第1期82-98,共17页
We further consider the effect of rod strength by employing the compressible penetration model to study the effect of compressibility on hypervelocity penetration.Meanwhile, we define different instances of penetratio... We further consider the effect of rod strength by employing the compressible penetration model to study the effect of compressibility on hypervelocity penetration.Meanwhile, we define different instances of penetration efficiency in various modified models and compare these penetration efficiencies to identify the effects of different factors in the compressible model. To systematically discuss the effect of compressibility in different metallic rod-target combinations, we construct three cases, i.e., the penetrations by the more compressible rod into the less compressible target, rod into the analogously compressible target, and the less compressible rod into the more compressible target. The effects of volumetric strain, internal energy, and strength on the penetration efficiency are analyzed simultaneously. It indicates that the compressibility of the rod and target increases the pressure at the rod/target interface. The more compressible rod/target has larger volumetric strain and higher internal energy. Both the larger volumetric strain and higher strength enhance the penetration or anti-penetration ability. On the other hand, the higher internal energy weakens the penetration or anti-penetration ability. The two trends conflict, but the volumetric strain dominates in the variation of the penetration efficiency, which would not approach the hydrodynamic limit if the rod and target are not analogously compressible. However, if the compressibility of the rod and target is analogous, it has little effect on the penetration efficiency. 展开更多
关键词 COMPRESSIBILITY hypervelocity penetration Equation of state(EOS) SHOCKWAVE Bernoulli equation
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爆轰驱动膨胀管性能研究 被引量:8
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作者 周凯 汪球 +1 位作者 胡宗民 姜宗林 《航空学报》 EI CAS CSCD 北大核心 2016年第3期810-816,共7页
超高速流动一般指速度超过5km/s的流动,由于流动具有高焓高速的特点,模拟超高速流动的地面试验设备面临极大挑战。膨胀管(风洞)是少数几种具备超高速流动模拟能力的地面试验设备之一。中国科学院力学研究所高温气体动力学国家重点实验室... 超高速流动一般指速度超过5km/s的流动,由于流动具有高焓高速的特点,模拟超高速流动的地面试验设备面临极大挑战。膨胀管(风洞)是少数几种具备超高速流动模拟能力的地面试验设备之一。中国科学院力学研究所高温气体动力学国家重点实验室(LHD)通过将正向爆轰驱动技术和膨胀管结合在一起,建成了可实现最高速度10km/s超高速试验气流的爆轰驱动膨胀管(JF-16),并开展了典型模型试验。在此基础上对JF-16进行了改造升级工作,为其设计喷管增加了膨胀风洞运行模式,对其性能进行了相关试验测试研究。同时,对膨胀管相关数值方法进行了介绍,并开展数值模拟对试验状态进行辅助诊断和分析。 展开更多
关键词 超高速 爆轰驱动 膨胀管 性能研究 试验测试 数值模拟
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金属材料的超高速刨削研究进展 被引量:7
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作者 张倩 朱仁贵 +2 位作者 李治源 李鹤 金龙文 《兵器材料科学与工程》 CAS CSCD 北大核心 2013年第4期97-103,共7页
综述国外40多年来金属材料超高速刨削研究进展情况。从试验研究和仿真研究两方面总结和分析了速度、材料特性、冲击角度等因素对超高速刨削的影响,重点阐述了刨削冲击形成机理及刨削抑制方法的研究现状。提出了下一步发展方向的建议。
关键词 金属材料 刨削 超高速 轨道炮 研究进展
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基于物质点法的轨道炮刨削机理三维数值研究 被引量:7
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作者 吴金国 林庆华 +3 位作者 弯港 金涌 李海元 栗保明 《爆炸与冲击》 EI CAS CSCD 北大核心 2017年第2期307-314,共8页
基于轨道炮结构特点以及冲击热力学理论,采用物质点法建立了轨道微颗粒诱发刨削的三维模型,模拟了轨道刨削的形成过程,并对其产生机理与影响因素进行了分析。结果表明:电枢与轨道的局域高速冲击产生瞬时的能量交换,形成的高热高压金属... 基于轨道炮结构特点以及冲击热力学理论,采用物质点法建立了轨道微颗粒诱发刨削的三维模型,模拟了轨道刨削的形成过程,并对其产生机理与影响因素进行了分析。结果表明:电枢与轨道的局域高速冲击产生瞬时的能量交换,形成的高热高压金属流对轨道表面的斜侵彻作用形成了刨坑;刨削的产生存在速度阈值,超过速度阈值,随着电枢速度增加,刨削越严重;低于速度阈值,可产生轨道擦伤;减小轨道表面微颗粒尺寸、增加电枢头部倾角均可降低刨削损伤。 展开更多
关键词 冲击动力学 物质点法 轨道炮 刨削 超高速
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Characteristics structure analysis on debris cloud in the hypervelocity impact of disk projectile on thin plate 被引量:6
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作者 Chun-bo Zhang De-ning Di +1 位作者 Xiao-wei Chen Ken Wen 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2020年第2期299-307,共9页
In this paper,the gauge points setting is introduced in the SPH simulation to analyze the debris cloud structure generated by the hypervelocity impact of disk projectile on thin plate.Compared with the experiments,mor... In this paper,the gauge points setting is introduced in the SPH simulation to analyze the debris cloud structure generated by the hypervelocity impact of disk projectile on thin plate.Compared with the experiments,more detailed information of the debris cloud structure can be classified from the numerical simulation.However,due to the solitary dispersion and overlap display of the particles in the SPH simulation,accurate comparison between numerical and experimental results is difficult to be performed.To track the velocity and spatial distribution of the particles in the debris cloud induced from disk and plate,gauge points are locally set in the single-layer profile in the SPH model.By analyzing the gauge points’spatial coordinate and velocity,the location and velocity of characteristic points in the debris cloud are determined.The boundary of debris cloud is achieved,as well as the fragments distribution outside the main structure of debris cloud. 展开更多
关键词 hypervelocity impact DEBRIS cloud SPH method Particle GAUGE points Motion CHARACTERISTICS
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超高速飞行弹箭气动烧蚀数值模拟研究 被引量:6
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作者 王中原 史金光 《南京理工大学学报》 EI CAS CSCD 北大核心 2003年第5期595-602,共8页
超高速弹箭存在的气动加热烧蚀现象会严重影响其外弹道特性。该文针对此类弹箭 ,旨在建立完善的气动加热、烧蚀模型 ,通过应用小扰动理论研究了弹 -翼间的气动干扰、采用轴对称比拟的方法考虑了有攻角 (非对称 )情况、引入热化学反应建... 超高速弹箭存在的气动加热烧蚀现象会严重影响其外弹道特性。该文针对此类弹箭 ,旨在建立完善的气动加热、烧蚀模型 ,通过应用小扰动理论研究了弹 -翼间的气动干扰、采用轴对称比拟的方法考虑了有攻角 (非对称 )情况、引入热化学反应建立了高温下的烧蚀准则。结合实例 ,对完善的气动加热、烧蚀模型进行了数值求解 ,并依据仿真结果归纳出一些烧蚀规律 ,对开展这方面研究有一定指导意义。 展开更多
关键词 超高速 弹箭 气动加热 烧蚀
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舰载电磁轨道武器的技术分析 被引量:5
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作者 巨兰 张碧雄 《舰船科学技术》 2009年第9期74-77,共4页
电磁轨道武器是一种利用电磁能推力的新概念动能武器,具有发射初速高、飞行时间短、毁伤效果好等技术性能优势。在简述未来海军电磁轨道武器火力支援工作原理的基础上,着重分析了该武器系统的射程、能源需求、技术优势,为武器系统的具... 电磁轨道武器是一种利用电磁能推力的新概念动能武器,具有发射初速高、飞行时间短、毁伤效果好等技术性能优势。在简述未来海军电磁轨道武器火力支援工作原理的基础上,着重分析了该武器系统的射程、能源需求、技术优势,为武器系统的具体实用装备提供了技术分析,并介绍了美海军未来的装备设想,最后分析了舰载电磁轨道武器的研究重点和启示。 展开更多
关键词 电磁轨道武器 超高速 电磁发射 动能 新概念武器
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Experimental investigation of spectral evolution in flash radiation by hypervelocity impact on aluminum plates
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作者 Xing Chen Yonggang Lu +1 位作者 Zhiwen Li Zhonghua Cui 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2024年第7期96-110,共15页
In this study,a series of hypervelocity impact tests were carried out based on a two-stage light gas gun,and the sequence spectrum and radiation evolution data of the impact products under different impact conditions ... In this study,a series of hypervelocity impact tests were carried out based on a two-stage light gas gun,and the sequence spectrum and radiation evolution data of the impact products under different impact conditions were obtained.The diameter of the projectile is 3-5 mm,the impact velocity is 3.13-6.58 km/s,and the chamber pressure is 0.56-990 Pa.The spectrum of ejected debris cloud in the 250-310 nm band were obtained using a transient spectral measurement system and a multi-channel radiometer measurement system.The test results reveal that the flash radiation intensity increases as a power function with the kinetic energy of the impact.Furthermore,the peak value of the line spectrum decreases as the chamber vacuum degree increases,while the radiation width gradually expands.The line spectrum in the spectral characterization curve corresponds to the ejected debris clouds splitting phase,which does not produce significant line spectrum during material fragmentation and is dominated by the continuum spectrum produced by blackbody radiation.There will appear one or three characteristic peaks in the flash radiation time curve,the first and second peaks correspond to the penetration phase and the third peak corresponds to the expansion phase of the ejected debris clouds on the time scale,the first and second peaks are more sensitive to the chamber vacuum degree,and when the pressure is higher than 99 Pa,the first and second characteristic peaks will disappear.The radiant heat attenuation of the flash under different impact conditions is significantly different,the attenuation exponent has a power function relationship with the impact velocity and the chamber vacuum degree,while the attenuation exponent has a linear relationship with the diameter of the projectile,the specific expression of the attenuation exponent is obtained by fitting.The findings from this research can serve as a valuable reference for remote diagnostic technologies based on flash radiation characteristics. 展开更多
关键词 hypervelocity impact Flash radiation EVOLUTION Spectral characteristics Damage evaluation
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