对刚体转动实验方法的研究与改进

本文讨论了改进刚体转动实验中造成误差的方法。     

Fluid flow due to combined convection in lid-driven enclosure having a circular body

The present work is aimed to study mixed convection heat transfer characteristics for a lid-driven air flow within a square enclosure having a circular body. Flows are driven by the left lid, which slides in its own plane constant velocity. This wall is isothermal and it moves up or down in y direction while the other walls remain stationary. The horizontal walls are adiabatic. The cavity is differentially heated and the left wall is maintained at a higher temperature than the right wall. Three different temperature boundary conditions were applied for the inner cylinder as adiabatic, isothermal or conductive. The computation is carried out for wide ranges of Richardson numbers, diameter of inner cylinder and center and location of the inner cylinder. It was found that the most effective parameter on flow field and temperature distribution is the orientation of the moving lid. The circular body can be a control parameter for heat and fluid flow. An interesting obtained result that the thermal conductivity becomes insignificant for small values of diameter of the circular body.     

Using quaternion matrices to describe the kinematics and nonlinear dynamics of an asymmetric rigid body

A set of four quaternion matrices is used to represent the equations of finite rotation theory and to describe the kinematics and nonlinear dynamics of an asymmetric rigid body in space. The results obtained are tested in setting up direction-cosine matrices, calculating three-index symbols, establishing the relationship between the components of angular velocity in body-fixed and space-fixed frames of reference, and using a set of three independent rotations. Euler–Lagrange equations and a set of four quaternion matrices are used to construct a block-matrix model describing the nonlinear dynamics of a free asymmetric rigid body in three-dimensional space. The model gives the matrix Euler’s equations of motion and other special cases. Algorithms adapted to use in a numerical experiment are developed Translated from Prikladnaya Mekhanika, Vol. 45, No. 2, pp. 133–143, February 2009.     

热、机械载荷作用下夹杂对应力强度因子的影响

推导了远场应力、热应力耦合作用下含夹杂裂纹体的应力强度因子求解公式,改进了体积力法中的裂纹面合力平衡条件,将应力强度因子的求解归结为解一组积分方程,再将积分方程转化为线性方程组进行数值求解。算例分析结果表明方法正确、有效。将该算法应用于含Al2O3夹杂的FGH95材料应力强度因子分析中,计算结果表明热应力对应力强度因子影响很小。     

A 20 nm gate-length ultra-thin body p-MOSFET with silicide source/drain

As the scaling of CMOS transistors extends to the sub-20 nm regime, the most challenging aspect of device design is the control of the off-state current. The traditional methods for controlling leakage current via the substrate doping profile will be difficult to implement at these dimensions. A promising method for controlling leakage in sub-20 nm transistors is the reduction in source-to-drain leakage paths through the use of a body region which is significantly thinner then the gate length, with either a single or a double gate. In this paper we present ultra-thin body PMOS transistors with gate lengths down to 20 nm fabricated using a low-barrier silicide as the source and drain. Calixarene-based electron-beam lithography was used to define critical device dimensions. These transistors show 260 μ A μ m ^{− 1}on-current and on/off current ratios of 10⁶, for a conservative oxide thickness of 40 Å and | V_g − V_t| = 1.2 V. Excellent short-channel effect, with only 0.2 V reduction in | V_t| is obtained in devices with gate lengths ranging from 100 to 20 nm.     

钠原子双激发［2p,3s］→［4p,kl］光电离截面计算

用多体微扰理论和原子体系图示法,研究和讨论了钠原子双激发 ［2p,3s］→［4p,kl(kp+kf)］并计算了钠原子的光电离激发截面,计算结果与实验结 果相符。     

钠原子双激发［2p，3s］→［5s，kl］ 光电离截面计算

用多体微扰理论和原子体系图示法,研究和讨论了钠原子双激发［2p, 3s］→［5s,kl (ks+kd)］并计算了钠原子的光电离激发截面,计算结果与实验结果相符 。     

纳米粒子的电容

纳米粒子的电容对由纳米点陈列所形成的单电子器件是一个十分重要的参数。基于少体理论,提出了计算纳米粒子量子点充电电容的理论模型,由此可以预测出室温下出现库仑台阶等单电子现象的最大纳米粒子粒径。采用简谐势模型计算模拟了CdS、PbS半导体纳米粒子的充电电容,发现CdS、PbS纳米粒子的尺寸上限为11与5 nm。理论计算结果与实验相吻合。     

The solving problem and the difference solving process for the shear of a bounded elastic bodies

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直升机下落碰撞的动力学响应研究

利用碰撞弹簧概念,结合多柔体系统动力学方法,建立了多体系附落碰撞的动力学模型。并通过求出响应,可详细描述碰撞过程。