金属材料再加载“准弹性”响应的实验验证

从连续介质力学理论看，当材料发生屈服后处于上屈服面，对处于上屈服面的材料进行再加载，将沿着上屈服面，依然发生塑性流动，不可能存在弹性响应。Asay则认为冲击压缩后的材料并非处于上屈服面，由此对处于冲击压缩态的材料进行卸载或再加载，可以观测到弹-塑性转变。国内部分人认为，实验观测到的弹性响应可能是LiF窗口（其冲击阻抗低于Al或其他高阻抗样品的冲击阻抗）反射的稀疏波所致。为了澄清对上述问题的观点，通过低阻抗样品的冲击实验，在消除冲击波在样品／窗口界面反射的稀疏波干扰的情况下，     

冲击压缩下非均质脆性固体的弛豫破坏研究

通过平板冲击实验研究了富含微缺陷的非均质脆性固体的冲击压缩响应特性.选取“强角闪石化橄榄二辉岩”作为样品材料，利用激光速度干涉仪测量样品后自由面的速度历史，在冲击加载应力远低于样品材料Hugoniot弹性极限的条件下，观测到了表征破坏波出现的再加载信号，并且该破坏波的速度远大于玻璃中破坏波的速度，以接近于冲击波的速度在样品内向前传播，其形成机理与玻璃样品中的破坏机理不同，称之为“就位扩展机理”.采用同一冲击加载应力(～3.9GPa)作用于不同厚度的样品,获得了破坏波穿过样品的运动过程，确定出样品中破坏波的轨迹线近似为一条不过原点的直线，相应的产生此破坏波的弛豫时间约为0.5 μs.     

FeMnNi合金冲击相变与卸载逆相变历程研究

采用VISAR测试技术,将正向加载和逆向加载实验相结合,研究了不同加载压力下FeMnNi合金的冲击相变和卸载逆相变历程.结果表明:冲击加载压力与冲击相变阈值之差小于逆相变阈值时,即0＜σp-σt＜σn,FeMnNi合金发生α→ε相变,加载段呈现弹性波、塑性波和相变波三波结构,塑性波在自由面反射稀疏波使FeMnNi合金完...     

动高压下拉格朗日声速的测定及其应用

 通过实时记录冲击加载—再加载和冲击加载—卸载波的粒子速度剖面,得到了再加载和卸载波在93W合金中传播的拉格朗日声速。通过拉格朗日声速从准弹性到纯塑性的转化,获得了材料在一次冲击终态时的剪应力、剪切模量以及考虑了剪应力修正后的93W合金的冲击绝热关系。     

铝的动态屈服强度测量及再加载弹性前驱波的形成机理分析

利用激光干涉测速技术(VISAR)测量LY12铝合金在20—34 GPa冲击压力下经历加载-卸载和加载-再加载过程的样品/窗口界面粒子速度剖面,采用AC方法确定了具有较高精度的动态屈服强度值.实验结果和文献发表的数据具有较好的一致性.通过以平面焊接方式制作组合飞片,克服了组合飞片在气炮发射过程中可能发生分离的技术困难,使铝的动态屈服强度测量压力范围从22 GPa扩展到了34 GPa.同时,根据对不同实验条件下的加载-再加载过程的比较,对再加载弹性前驱波的形成机理进行了讨论,认为位错是形成该现象的主要原因. 关键词： 动态屈服强度 AC方法 弹性前驱波 VISAR     

铝的动态屈服强度测量及再加载弹性前驱波的形成机理分析

利用激光干涉测速技术(VISAR)测量LY12铝合金在20—34 GPa冲击压力下经历加载-卸载和加载-再加载过程的样品/窗口界面粒子速度剖面，采用AC方法确定了具有较高精度的动态屈服强度值.实验结果和文献发表的数据具有较好的一致性.通过以平面焊接方式制作组合飞片，克服了组合飞片在气炮发射过程中可能发生分离的技术困难，使铝的动态屈服强度测量压力范围从22 GPa扩展到了34 GPa.同时，根据对不同实验条件下的加载-再加载过程的比较，对再加载弹性前驱波的形成机理进行了讨论，认为位错是形成该现象的主要原因.     

平板冲击下氧化铝陶瓷弹性前驱波衰减的细观机理

利用一级轻气炮开展了不同厚度氧化铝陶瓷样品的平板冲击压缩实验,并借助激光速度干涉仪(VISAR)测试了样品的自由面速度历程.根据自由面速度历程确定了不同厚度氧化铝陶瓷样品的Hugoniot弹性极限值,结果显示,冲击压缩下氧化铝陶瓷中存在弹性前驱波衰减现象.进一步基于氧化铝陶瓷的细观结构扫描电镜(HEL)图像,分析了氧化铝陶瓷的细观结构特征,构建了含晶相、玻璃相等细观特征的力学模型.数值模拟冲击压缩加载下氧化铝陶瓷细观结构的力学响应过程,从细观层次上分析了弹性前驱波衰减现象的产生机理,指出冲击压力低于HEL时材料的细观损伤引起的能量耗散以及前驱波在细观结构晶界处反射和透射引起的能量分散过程是其产生的主要原因.     

冲击加载下20钢中弹性前驱波衰减与应力松弛行为实验研究

 通过改变样品厚度，对平面冲击加载下20钢的弹性前驱波的波幅衰减和应力松弛进行了实验研究。采用激光速度干涉测速仪（VISAR）实测了样品后自由面速度历史，采样频率达到1 ns，保证了实验结果的准确性。实验结果显示：Hugoniot弹性极限随着传播距离呈指数衰减，在所研究的样品厚度范围内，Hugoniot弹性极限减小了44%；应力松弛行为和弹性前驱波的上升沿时间也依赖于传播距离；冲击加载的强度对材料动态屈服行为的影响很小。     

固体炸药的磁驱动准等熵压缩实验研究

较宽压力范围内未反应炸药的本构关系和状态方程对于深入和精确认识压缩波作用下炸药组分间相互作用的力学过程和起爆热点的形成机制具有重要意义。较之冲击压缩,磁驱动准等熵压缩加载(无冲击压缩)是获取较宽压力范围内未反应炸药的动态压缩力学特性更有效的手段。基于大电流产生的电磁力作用原理,在国内率先实现了炸药的磁驱动无冲击压缩实验技术。通过对负载电极、炸药样品参数的优化设计和安装工艺的控制,实现了5 GPa载荷内JO-9159炸药的磁驱动准等熵压缩加载。基于激光位移干涉测量技术和Lagrange数据处理方法,获得了JO-9159炸药的速度响应历史和准等熵压缩线。所得结果与文献数据进行了比较,结果表明,在实验压力范围内,JO-9159炸药的等熵压缩线与PBX9501炸药的等熵压缩线一致。     

冲击载荷下非晶态碳材料的动态响应模型研究

 在一维应变冲击加载条件下，采用两个石英压力传感器进行了双值应力历史测量，对非晶态碳材料的动态响应特性进行了分析研究。研究结果表明，非晶态碳材料的冲击响应是简单稳定的，在试验冲击应力范围内为非线性弹性响应，Hugoniot曲线呈上凸的，表明材料内部传播的不是一个冲击波而是一簇压缩波，因此可采用特征线方法来解该冲击波问题，并用Riemann积分法对冲击应力过程进行修正，得到材料更精确的Hugoniot方程。还采用COPS程序对该材料的冲击响应过程进行了数值模拟，数值模拟曲线与试验曲线是很吻合的。表明采用Riemann积分法处理是合理的，此方法可以在VISAR测量中得到应用。     

双屈服法测定93W合金的屈服强度

 用组合飞片技术以实现对待测材料93W合金进行加载-再加载和加载-卸载，并用VISAR（Velocity Interferometer System for Any Reflector）测试方法和高速数值示波器记录样品-窗口界面的粒子速度，通过上下屈服面法对实验数据进行处理，从而推出93W在冲击压力分别为16、32和96 GPa三个压力点下的屈服强度为：1.8、2.6和4.9 GPa。得到了93W合金在高压下材料屈服强度随冲击压力的增大而增大，但其与冲击压力的比值则随冲击压力的增加而减小的变化规律。     

Collective properties of defects,multiscale plasticity,and shock induced phenomena in solids

A statistically based approach is developed for the construction of constitutive equations that provides linkages between defect-induced mechanisms of structural relaxation, thermally activated plastic flow, and material response to extreme loading conditions. The collective properties of defects have been studied to establish the interaction of multiscale defect dynamics and plastic flow, and to explain the mechanisms leading to the universal self-similar structure of shock wave fronts. Pn explanation for structural universality of the steady-state plastic shock front (the four power law) and the self-similarity of shock wave profiles under reloading (unloading) is proposed. Structural characterization under transition from thermally activated dislocation glide to nonlinear dislocation drag effects is developed in terms of scaling invariants (effective temperatures) related to mesodefect induced morphology formed during the different stages of plastic deformation.     

气炮加载实验中光学窗口透射率测量技术及其应用

报道一种用于气炮加载条件的窗口透射率测量技术。该技术将一种激发电压低(4.5 V)、响应时间快(约500 ns)、输出功率稳定的半导体脉冲光源设置在弹丸内部,在碰靶前激发出光,作为照明光源,用于观测透明样品/窗口在加载过程中的透射率变化。将该技术用于石英玻璃冲击透明性研究,发现石英玻璃在经冲击压缩再卸载到水的过程中,其透射率下降了近30%,该结果不支持文献中所给出的液态水压致固化的解释。     

金属冲击温度的辐射法测量问题

 金属的冲击温度及熔化温度测量对构建其完全状态方程具有重要意义。简要综述了用于金属冲击温度及熔化温度辐射法测量的一维热传导理想界面模型和非理想界面模型,并着重对模型中明示或隐含的关键假定的合理性、影响金属冲击温度与熔化温度结果的主要因素进行了分析、讨论,以期对实验数据有一个合理的评估。还讨论了求解理想和非理想界面模型一维热传导方程界面温度时所隐含的冲击压缩下热导率不随温度而变、冲击压缩下金属样品/窗口界面辐射的灰体假定,以及窗口材料的透明性、非理想界面模型中表观界面温度的修正、动载条件下金属高压熔化温度的测量、界面的非Flourier热传导等问题。分析结果表明,目前采用辐射法测量大致可以得到冲击温度,在发生熔化的情况下可获得熔化温度,但离精密测量的要求还有较大差距。     

Problems of shock temperature measurements for metals by using optical radiometry method

Abstract

Several problems encountered in shock temperature measurements for metals using optical radiometry were discussed in detail. The influences of the driver/film gap upon the observed interface temperature history were formulated analytically, and the temperature relaxation behaviors at the film/window interface were also characterized. We found that the energy deposition at the driver/film gap would influence to varied degrees the film/window interface temperature profile unless the film deposited on the window can be regarded to have an infinite thickness. Modeling calculations showed that at shock pressures of a few megabars, the observed interface temperature of iron would be at least 300–600 K higher, relative to the prediction from the Grover model, provided that the gap and film were both 1 ～ 2 pm thick. Additionally, a metal-plate sample was used to measure a reliable shock temperature based on one-dimensional heat conduction model for the plate-sample(driver)/ pm-gap/window setup we proposed. Preliminary measured results for a meteoritic iron sample (kamacite, with Fe 93.65 wt.% and Ni 6.35 wt.%) using a disc sample showed that this method was practical and effective. Finally, the “heat-resistance model” proposed by Tang et al., and the experimental measurement of the heat conductivity for a transparent window (sapphire or LiF crystal) at megabar shock pressures were discussed and commented on as well.     

Generation of laser-driven flyer dominated by shock-induced shear bands: A molecular dynamics simulation study

High-power pulsed lasers provide an ingenious method for launching metal foils to generate high-speed flyers for high-pressure loading in material science or aerospace engineering.At high-temperature and high-pressure laser-induced conditions,the dynamic response of the metals and the mechanism of flyer formation remain unclear.In this study,the overall process of the laser-driven aluminum flyer,including laser ablation,rupture of metal foil,and the generation of the flyer was investigated by molecular dynamics combined with the two-temperature model.It was found that under high laser fluence(over 1.3 J/cm;with 200-fs laser pulse duration),the laser induced a shock wave with a peak pressure higher than25 GPa,which led to shear bands expanding from the edge of the laser ablation zone in the foil.Compared with the cases of low laser fluence less than 0.5 J/cm^-1,the shear band induced by high laser fluence promotes the rupture of the foil and results in a high-speed flyer(>1 km/s)with better flatness and integrity.In addition,the shock wavefront was found to be accompanied by aluminum crystal phase transformation from face-centered cubic(FCC)to body-centered cubic structure.The crystal structure reverts with the decrease of pressure,therefore the internal structure of the generated flyer is pure of FCC.The results of this study provide a better understanding of the laser-induced shock effect on the foil rupture and flyer quality and forward the development of the laser-driven flyer.     

冲击波压缩PVDF膜的电响应研究

 应用冲击加载技术,研究了PVDF膜在与其极化矢量方向平行的冲击波压缩下的冲击电响应。通过实验和数值模拟得到了PVDF释放电荷q(t)与冲击波压力p(t),给出了峰值电荷q_max与峰值压力p_max的关系,建立了PVDF膜的冲击电响应的理论模型及数值模拟方法。     

两种光纤探针在冲击波作用下的时间响应特性

 对冲击波参数的测量开发了两种光纤探针，以满足强电磁环境和冲击压力较低的情况。一种是冲击自发光光纤探针，另一种是闪光隙光纤探针。这两种光纤探针分别利用融凝石英在受到冲击压缩时发光和氩气（或空气）隙在受到压缩时会产生很强的光辐射的机理研制而成的。自发光光纤探针在大于70 GPa冲击压力下，其信号上升时间在1~3 ns之间；闪光隙光纤探针在10～30 GPa的冲击压力下，其信号上升时间稳定在2~7 ns之间。     

Reshock Response of 2A12 Aluminum Alloy at High Pressures

By means of mounting the specimen on a low-impedance buffer, reshock experiments were carried out on a 2A12 almninum alloy up to shock stresses＇ of 67.6 GPa. Reshock wave profiles from the initial shock stresses of 60.9-67.6 GPa were measured with a velocity interferometer, and it shows that the 2A12 aluminum alloy characterizes as quasi-elastic response during recompression process. The Lagrange longitudinal velocities along the reloading path from initial shock state were obtained from two shots of experiments, while the bulk velocities at corresponding shock stresses were determined via extrapolating from the public reported unloading plastic sound velocities. Combining the reshock and the release experimental results, the yield strength of 2A12 aluminum alloy at shock stress of 60.9 GPa was estimated to be about 1.7GPa.