碰撞问题浅谈

碰撞是一个重要的物理模型，但同学们对此模型的认识和理解有些困难，下面对此问题进行讨论．     

Effect of Nuclear Binding Energy to K Factor

We modify the square of virtual photon four-momentum by using nuclear binding energy formula, and calculate the effect of nuclear binding energy to K factor and Compton subprocess and annihilate subprocess in A-A collision Drell-Yan process. The outcome indicates that the effect of nuclear binding energy to K factor is obvious in little x region and it would disappear gradually as x increases.     

Langevin Simulation of Non-Uniform Granular Gases

We present and study a fractal model of a non-uniform granular system for the first time, based on which wenumerically solve the dynamics actions in the system successfully in one-dimensional case. The multi-mixture is composed of N different particles, whose granularity distribution has the fractal characteristic. The particles are subject to inelastic mutual collisions and obey to Langevin equation between collisions. Far from the equilibrium,i.e. the given typical relaxation time τ of the driving Brownian process is much larger than the mean collision time τc, the results of simulation indicate that the degree of inhomogeneity in the granularity distribution signed by the fractal dimension D of size distribution has great influence on the dynamics actions of the system. The velocity distribution deviates obviously from the Gaussian distribution and the particles cluster more pronouncedly with the larger value of D in the system. The velocity distribution and spatial clnsterization change with D are presented.     

CO（ a）+ NO（X）传能体系中的新传能通道

在相对碰撞平动能为 0 .0 5eV的分子束实验条件下 ,研究了亚稳态CO(a) +NO(X)的E E传能通道 .通过测量和分析交碰区的传能发射光谱 ,在 780和 860nm处观测到了NO(b -a)跃迁Ogawa带的△v =+ 4和△v =+ 3序的发射光谱 .从而首次在实验上直接证实了传能过程中第四通道的存在 (CO (a) +NO(X)→CO (X) +NO(b) ) .这一通道的发现解释了前人测量到的在CO(a)与NO(X)碰撞传能过程中CO(a)的猝灭速率远大于NO(A ,B)生成速率的实验结果 ,并进一步证实了这一“经典”E E传能体系为电子交换机理的传能观点     

确定SHPB实验中延迟时间的曲线拟合法

 利用已知的试件密度，用预估的透射波与实测的透射波进行早期形状比较，确定试件弹性波速度，进而确定了SHPB试验数据处理时的延迟时间。     

智能延迟触发产生器设计

在弹道测量、高速飞行物碰撞实验（如太空的‘垃圾’碎片对飞行的卫星、飞行舱的损害研究）及其它的类似实验中，需要准确测量飞行物碰撞前的一些状态：如速度、飞行姿态、断裂等情况，并且希望得到在碰撞前很短的距离处测量的数据。那么，在使用X光的阴影照相技术中有关X光机的触发问题就显得更加重要；如果X光机提前触发，此时飞行物还未进入照相区域或者离碰撞区的距离还远，则记录不到弹丸的X光图像或者位置不理想而造成数据不够准确；如果X光机延迟过多触发，则因已碰撞而无法获得碰撞前的状态参数：所以，X光机的触发时刻必须准确才能保证获得物体在希望位置处的X光阴影图像，并且降低实验成本。     

DUAL RECIPROCITY HYBRID BOUNDARY NODE METHOD FOR THREE-DIMENSIONAL ELASTICITY WITH BODY FORCE

Combining Dual Reciprocity Method （DRM） with Hybrid Boundary Node Method （HBNM）, the Dual Reciprocity Hybrid Boundary Node Method （DRHBNM） is developed for three-dimensional linear elasticity problems with body force. This method can be used to solve the elasticity problems with body force without domain integral, which is inevitable by HBNM. To demonstrate the versatility and the fast convergence of this method, some numerical examples of 3-D elasticity problems with body forces are examined. The computational results show that the present method is effective and can be widely applied in solving practical engineering problems.     

Na离子和Cl离子引起He原子直接多重电离过程的研究

利用2～8 MeV的Naq+、Clq+(q=2,3,4,5)轰击氦原子,对碰撞的直接多重电离过程进行研究.实验采用反冲离子-散射离子飞行时间符合技术,通过反冲离子飞行时间谱区分不同价态反冲离子;利用静电偏转和位置灵敏探测技术区分不同电荷态散射离子;结合CAMAC-PC多参数获取系统得到一定价态散射离子所对应的反冲离子电荷态分布谱;经分析该谱得到直接多重电离截面与直接单电离截面之比R21.讨论了R21随入射离子速度和电荷态的变化关系.     

Experimental and Theoretical Evidence for the Existence of Broad Forbidden Gaps in the Three—Component Composite

The influence of localized resonance on the properties of band-gaps of the two-dimensional periodic composite are analysed numerically and experimentally by comparing the two-component phononic crystal with the three-component one. The three-component composite which exhibits localized resonance in the elastically soft coating ring is composed of a square array of coated cylinders embedded in an epoxy resin. The coated cylinders consist of a steel inner core and a rubber coating, which has much smaller wave velocity and mass density than the matrixand tile inner material. Tile measured transmission power of tile three-component composite drops to the noise level in a broad ultrasonic frequency interval in contrast to the binary composite, which is in good agreement with the calculation using the finite element method.     

U-6Nb合金机加过程中的塑性变形及其消除方法

国外早在20世纪80年代初就已发现U-6Nb合金在机械加工过程中的尺寸不稳定性问题，并认为该现象可能是由于该合金所具有的高密度孪晶、低屈服应力及热弹性马氏体相变等特性共同作用的结果。结合U-6Nb合金的组织结构、机械加工工艺及热处理工艺，探讨U-6Nb合金在机械加工过程中产生塑性变形的原因并利用其具有形状记忆效应这一特性，采用200℃时效的方法探索其变形的消除方法。