共查询到17条相似文献,搜索用时 125 毫秒
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激光驱动带窗口宏观飞片特性实验研究 总被引:3,自引:0,他引:3
利用激光驱动带窗口宏观高速飞片技术可以实现对材料的一维加载,特别适合开展材料的高压状态方程及高应变率下材料的动态力学特性研究。利用小型脉冲YAG激光器进行了驱动飞片技术研究。开展了飞片结构对飞片力学参数影响的实验,结果表明:复合靶飞片的能量耦合效率比单膜结构飞片具有较大的提高,平均速度提高约15%~30%。同时,飞片的平面性和完整性也有明显的改善。实验中测量了飞片的启动弛豫时间,结果显示:飞片的启动弛豫时间为5~10 ns。利用多通道光纤阵列开展了飞片的平面性测量。实验结果表明,在约1.0 mm的范围内,飞片的时间分散性为20~30 ns。利用高灵敏度激光干涉技术,对飞片速度历史进行了测量,结果表明,飞片在前20 ns就加速到最终速度的90%以上。 相似文献
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以激光驱动飞片速度场诊断为例,展示线面同时成像任意反射面速度干涉仪(VISAR)技术在超高速碰撞研究中的应用前景。将传统VISAR改为成像干涉结构,用变像管扫描相机和高速光电分幅相机分别记录作为信号载体的梳状干涉条纹随时间的变化,实现靶面一条线上各点速度历程和多个时刻二维靶面上所有点速度相对分布的测量。所研制的线面同时成像VISAR具有10μm的空间分辨和约15m/s的速度分辨能力。用其测量了激光驱动铝膜飞片的速度场,直观给出飞片的演化发展过程。实验结果表明,线面同时成像VISAR技术可以为激光驱动飞片、超高速碰撞等领域的理论研究和数值模拟提供有效比对实验数据。 相似文献
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阻抗匹配法是激光状态方程实验重要的测量方法,阻抗匹配靶的质量与靶参数的测量精度直接影响状态方程实验数据的可靠性与精度。因此,2004年致力于高质量铝铜阻抗匹配靶的制作,并努力提高靶参数的测量精度。 相似文献
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在准真空环境下,采用高功率密度的调Q-Nd:YAG激光照射固体铝靶表面,测量了不同入射激光强度下气化靶物质对靶的冲量.通过分析不同情况下激光与固态靶、气化物质的作用机理,采用流体力学理论和三维有限差分的计算方法,对不同激光强度情况下气化物质对靶产生冲量的过程进行了数值模拟,将模拟计算所得结果与实验测量结果进行了比较和分析,进而对实验结果进行了解释.由数值模拟结果与实验结果的一致性可见,本文采用的模型能反映激光作用下固体靶力学响应的物理过程. 相似文献
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We present the numerical calculation of the model of
aluminum flyer-vacuum-target with high power laser driving.The results show that the
parameters of laser and target's structure have great effects on the state of flyer and
the character of shock-waves in the target.If we select the parameters of laser and
target's structure reasonably, we can achieve approximately symmetric impact between flyer
and target;moreover,the shock-wave in the target has a stable area with a certain spatial
width.So,if we choose the three-step-target with a suitable thickness,we can approach an
absolute measurement of equation-of-state. 相似文献
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Numerical Simulation of the Response of an Aluminum Target Impacted by an Intense Laser Driven Flyer
1 Introduction Theimpacttechniqueofflyerdrivenbychemicalexplosiveandgasgunhasbeenusedtostudyhigh pressureequation of state (EOS)formanyyears[1] .Becausetheflyerisatalowenergydensityandentropyenhancementstateinthiscase ,itcaneasilyrecoveritsinitialstatebefo… 相似文献
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Numerical Simulation of the Response of an Aluminum Target Impacted by an Intense Laser Driven Flyer
Numerical calculations of the response of an aluminum target impacted by an aluminum flyer driven by an intense laser are presented. The state of the accelerated flyer and the characteristics of shock wave propagation in the target are described in detail. If the parameters of laser and flyer-target structure are selected reasonably, an approximately symmetric impact can be realized between the flyer and the target, also the shock wave in the target has a wide stable range. Therefore the absolute measurement for the equation of state (EOS) can be almost achieved in laser EOS experiments with the bothside-step-target of suitable thickness. 相似文献
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在激光驱动飞片研究中,飞片的加速特征是需要认识的关键问题之一。设计了强激光作用金属膜驱动飞片实验,采用聚偏氟乙烯(PVDF)压电薄膜测量了飞片到达不同距离的时间,计算得到飞片速度和加速度,分析激光能量对飞片加速性能的影响。基于Gurney能理论,建立了激光驱动飞片速度的计算模型,根据实验结果获得了激光能量损失系数和有效吸收系数,分析了激光能量和膜体厚度对飞片速度的影响。实验结果表明:不同激光能量下飞片的加速特征基本相似,激光能量变化对飞片的加速时间影响较小; 激光能量较大的情况下,膜体厚度对飞片最大速度、能量耦合系数的影响更显著; 当膜体超过一定厚度时,能量耦合系数不再增加。 相似文献
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Absolute distance measurements can be performed with an interferometric method that uses only a single tunable laser. This method has one major drawback, because a small target movement of the order of one wavelength during a measurement will be interpreted as a movement of one synthetic wavelength. This effect is usually mitigated by adding a second (nonscanning) laser. We show that absolute distance measurements can be performed with only one laser if the movements encountered are smooth, on the time scale of one measurement. In this case the movement errors can be compensated with a simple algorithm that combines several subsequent measurements. First experimental results show good agreement with theory. 相似文献
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Hyeonju Yu Vitalij Fedotov Wonkye Baek Jack J. Yoh 《Applied Physics A: Materials Science & Processing》2014,115(3):971-978
A laser driven flyer (LDF) system is designed to blast off a very small, thin flyer plate for impact on a target. When a Nd:YAG laser beam is focused through a transparent substrate onto thin metal, a fraction of the metal is ablated. The blow-off products being contained between the substrate and the flyer make the remaining thin film launch as a separate flyer. Some energy of the laser beam is lost by reflection at the boundary between substrate and metal because of the high reflectivity. By using a proper metal of high absorptance at 1.064 μm wavelength, the laser coupling to the flyer would define the system efficiency of a launch system. An effort is presented here to improve the coupling results in the enhancement of the flyer velocity for a given pulse energy. An optimum energy conversion between laser energy and kinetic energy of the flyer is achieved through a black paint coating technique as opposed to a more conventional means of a multi-layered approach requiring electron beaming or magnetron sputtering that are rather expensive and time consuming. The mini flyer flown under 1.4 km/s showed a controlled flight trajectory without fragmentation, suggesting that performance of this simple system is competitive to if not better than other attempts by the multi-layered LDF systems. 相似文献