On the behaviour characterization of metallic cellular materials under impact loading

This paper reviews the common mechanical features of the metallic cellular material under impact loading as well as the characterization methods of such behaviours. The main focus is on the innovations of various testing methods at impact loading rates.Following aspects were discussed in details.（1） The use of soft nylon Hopkinson/Kolsky bar for an enhanced measuring accuracy in order to assess if there is a strength enhancement or not for this class of cellular materials under moderate impact loading;（2） The use of digital image correlations to determine the strain fields during the tests to confirm the existence of a pseudo-shock wave propagation inside the cellular material under high speed impact： （3） The use of new combined shear compression device to determine the loading envelop of cellular materials under impact multiaxial loadings.     

THERMAL SHOCK OF SEMI-INFINITE BODY WITH MULTI-PULSED INTENSE LASER RADIATION

In order to investigate the thermal shock and the heat conduction property of a target under multi-pulsed laser radiation, analytic expressions of both temperature and thermal stress fields in the target are deduced on the basis of the non-Fourier conduction law and the thermo-elastic theory. Taking a stainless steel target as an example, we can solve the analytic expressions under appropriate boundary conditions by using the finite difference method and MATLAB software, and then reveal the evolution law of both surplus temperaturt, and thermal stress in the target. The results indicate that the temperature curves in the target irradiated by a multi-pulsed laser take on a delayed character in different sections away from the boundary, which is only affected by its relaxation time. The front of the stress wave is very steep in the non-Fourier numerical solutions, which presents an obvious thermal shock, so it is necessary to consider the non-Fourier effect of semi-infinite body under the high energy laser radiation.     

APPROXIMATE SOLUTIONS FOR TRANSIENT RESPONSE OF CONSTRAINED DAMPING LAMINATED CANTILEVER PLATE

The series composed by beam mode function is used to approximate the displacement function of constrained damping of laminated cantilever plates, and the transverse deformation of the plate on which a concentrated force is acted is calculated using the principle of virtual work.By solving Lagrange＇s equation, the frequencies and model loss factors of free vibration of the plate are obtained, then the transient response of constrained damping of laminated cantilever plate is obtained, when the concentrated force is withdrawn suddenly.The theoretical calculations are compared with the experimental data, the results show：both the frequencies and the response time of theoretical calculation and its variational law with the parameters of the damping layer are identical with experimental results.Also, the response time of steel cantilever plate, unconstrained damping cantilever plate and constrained damping cantilever plate are brought into comparison, which shows that the constrained damping structure can effectively suppress the vibration.     

爆炸与冲击动力学若干问题研究进展

介绍了爆炸与冲击动力学数值模拟领域近几年的研究重点及主要进展.包括材料本构关系、损伤破坏、冲击相变、射流和微喷等,其中材料本构关系的发展比较系统,有几个典型的模型可以参考,不仅应用广泛,而且有实验数据进行检验和对比.损伤模型只有唯象模型,虽然有不同的物理机制,但缺少直接的实验依据.射流的工程应用比较广泛,理论研究比较缺乏.微喷研究基本停留在定性阶段.随着实验技术及测量手段的发展,相关领域取得了一些令人欣慰的进展.     

基于ALE方法的飞机水面降落过程

为了研究飞机水面降落过程中的动态响应规律,采用arbitrary Lagrangian-Eulerian(ALE)方法开展了飞机水面降落的动力学分析。研究了飞机水面降落过程的速度变化规律,结果表明,降落速度和飞行速度在飞机入水的初始阶段变化较快,随后变化幅度趋于平缓。分析了不同降落速度、飞行速度和降落仰角下的机身结构响应,得到了飞机水面降落时结构响应随时间的变化规律。机身结构应力在入水的初始阶段达到最大值,随后迅速下降,最后保持稳定。飞机结构的最大变形也出现在入水的初始阶段,随后迅速回复到初始状态。对比了降落速度、飞行速度和降落仰角对飞机结构响应的影响程度,结果表明降落速度对结构响应的影响程度最大,降落仰角次之,飞行速度的影响最小。 更多还原     

动静组合加载下花岗岩的力学性能

在霍普金森试验系统上进行了花岗岩动静组合加载试验,获得了花岗岩在动静组合加载下的力学性能.试验结果表明:当动载不变,改变静栽大小,在弹性范围内,花岗岩强度随着静载增大而增大;当静载超过弹性极限时,花岗岩强度迅速降低;在其破坏过程中对冲击能量的吸收随静载增大而减小;变形模量呈现明显的两段特征.当静载不变,改变动载大小,花岗岩的强度随动载增大而增大;变形模量先随动载增大而增大,而后又突然变小,并不出现两段特征;在其破坏过程中对冲击能量的吸收随动载应变率的增大而逐渐增大.所得结果为岩爆、深部破岩等研究提供实验依据.     

谐和与宽带噪声联合激励下含分数导数型阻尼的Duffing振子的平稳响应

用广义谐和函数导出了含分数导数型阻尼的Duffing振子在谐和与宽带噪声联合作用下的随机平均方程,然后用有限差分法求解了平均FPK方程得到系统的随机稳态响应,研究了分数阶数对随机跳跃分岔影响。最后,通过与原方程MonteCarlo数字模拟结果的比较,验证了所得结果的正确性。     

冲击荷载下单层球面网壳的失效机理

为研究单层球面网壳在冲击荷载下的失效机理,在ANSYS/LS-DYNA中建立60m跨度K8型单层球面网壳与圆柱形冲击物的数值模型并进行数值分析,总结了网壳结构的4种失效模式。通过对失效全过程的分析,从能量的角度将失效过程分为能量施加、能量传递与损失、能量消耗3个阶段。之后分别从能量传递与杆件破坏形式2方面揭示了网壳的失效机理。能量分析表明:剩余能量(Elf)对结构最终动力响应及失效模式起决定作用,而Elf只是初始冲击能量中除去冲击物穿透损失与网壳局部破坏损失后的剩余部分。通过对杆件破坏形式的分析发现:杆件的破坏可能滞后于冲击荷载的作用,且杆件的破坏形式决定其传递能量的能力,当杆件发生拉伸破坏时,其强度被充分利用,传递的能量最多,Elf值较大,网壳整体破坏严重。杆件的破坏形式与Elf及网壳整体的失效模式间有很好的对应关系。     

撞击载荷下泡沫铝夹芯梁的塑性动力响应

应用泡沫金属子弹撞击加载的方式研究了固支泡沫铝夹芯梁和等质量实体梁的塑性动力响应。 采用激光测速装置和位移传感器测量了泡沫子弹的撞击速度和后面板中心点的位移-时间曲线,研究了加载 冲量、面板厚度和芯层厚度对夹芯梁抗冲击性能的影响。给出了泡沫铝夹芯梁的变形与失效模式,实验结果 表明结构响应对夹芯结构配置比较敏感,后面板中心点的残余变形与加载冲量、面板厚度呈线性关系。与等 质量实体梁的比较表明,泡沫铝夹芯梁具有更好的抗冲击能力。实验结果对多孔金属夹芯结构的优化设计具 有一定的参考价值。     

非对称圆环拍的特性研究

建立微小非对称圆环点冲击下拍的理论模型,通过实验验证其有效性。微小非对称圆环是分析大钟拍现象的简化模型,微小非对称圆环的每一对径向振动模态的固有频率非常接近,这对模态互相干涉下出现拍现象。最后利用拍的理论模型绘制沿圆周拍的分布图,详细分析拍的分布特性,为校正钟的拍频声提供理论依据。