新型有机锗倍半氧化物及硫化物的合成

已先后合成的倍半氧化物类及倍半硫化物类化合物的前体,即有机锗三氯化物中只含1个锗原子。为了考查从含2个锗原子的前体合成的有机锗倍半氧化物及硫化物的药物活性,我们合成了1类化合物及相应的倍半氧化物(2类)及倍半硫化物(3类),并合成了酰基苯胺化合物1_e、2_e及3_e。结果见表1。     

双峰倍增配平法用于同步、导数-同步荧光法同时测定邻羟基苯甲酸和间羟基苯甲酸

邻羟基苯甲酸（ｏＨＢＡ）和间羟基苯甲酸（ｍＨＢＡ）荧光光谱严重重叠，同步及导数技术虽使选择性有所改善，但仍不能完全分辨开重叠谱。用双峰倍增配平计算法结合同步、一阶导数－同步荧光法对双组分体系（邻羟基苯甲酸／间羟基苯甲酸，ｐＨ１２介质）同时测定。结合计算的两种测定方法精密度、回收率和不同组分间浓度比范围均优于一阶导数－同步荧光法。     

8,10-二炔廿五碳酸LB膜的周期结构

合成了8,10-二炔廿五碳酸,在玻璃片、石英片和镀金片上沉积了它的LB膜,X-射线衍射研究了LB膜的周期结构和聚合对它的影响。在2θ=1°—15°范围内观察到了多达7个布拉格衍射峰。由此计算了等同周期和分子在基片上的倾斜角。用分子模型计算了衍射峰强度,得到了与实验结果相符合的衍射峰强度奇偶起伏现象。     

分级周期梁结构的振动带隙特性优化研究

针对分级周期梁结构,进行了振动带隙特性优化研究,以期提高结构的减振性能.采用谱元法计算分级周期梁的频响曲线,并结合传递矩阵法计算结构的色散关系,将两种方法相结合来研究结构的振动带隙特性.构建带隙占比函数作为优化目标函数,将单胞结构的尺寸作为优化参数进行带隙特性优化.经过优化,使得在研究频段内带隙特性大大提高.通过与有限...     

随机ADMM算法及其在电力系统凸经济调度问题中的应用

针对电力系统中的一类凸经济调度问题,提出了随机ADMM算法,设计了周期循环更新规则和随机选择更新规则,证明了随机ADMM算法在周期循环更新规则下的收敛性,以及得出了在随机选择更新规则下按期望收敛的结论.数值实验结果表明该方法可以有效解决电力系统中的凸经济调度问题.     

大非球面镜的郎奇检验灵敏度理论研究及仿真分析

为了研究等间距直线条光栅的周期及其他相关参数的变化对大非球面镜朗奇检验法的影响,提出了一种评估郎奇检验灵敏度大小的新方法。其检验灵敏度定义为一个光栅周期所能检测到的镜面偏差大小能力。在朗奇检验的几何原理基础上,利用光线追迹法讨论了镜面偏差与朗奇光栅周期之间的关系,并以此推导出检验灵敏度公式,计算了抛物面镜的朗奇检测灵敏度。分析结果表明,如果给定镜子的规格参数及检验光路,朗奇检验灵敏度分别随着光栅周期间隔和半通光口径的变大而减小。     

基于透明陶瓷材料的激光研究进展

陶瓷激光器是一种以透明陶瓷材料作为增益介质的激光器.与单晶相比,透明陶瓷具有制备周期短和烧结温度低等优势,在激活离子高掺杂浓度下能保证良好的光学均匀性,且容易制备成各种大尺寸复合结构.近年在高功率和超短超强激光输出方面得到广泛应用,产生了一系列研究成果.回顾了陶瓷激光器的发展历程,总结了透明陶瓷在高功率、超短超强脉冲激...     

快速响应高压电源在KTP晶体极化反转中的应用研究

分析了KTP晶体电导率的特性,设计与研制出一种新型的高压脉冲放大器,可将任意信号发生器产生的信号线性放大,响应速度快,最高输出电压为4000V,最大输出电流为30mA,功率可达100W.用其在KTP晶体上进行多次极化反转实验,取得良好的实验结果.     

ACTIVE CONTROL OF A FLEXIBLE CANTILEVER PLATE WITH MULTIPLE TIME DELAYS

Active control of a flexible cantilever plate with multiple time delays is investigated using the discrete optimal control method. A controller with multiple time delays is presented. In this controller, time delay effect is incorporated in the mathematical model of the dynamic system throughout the control design and no approximations and assumptions are made in the controller derivation, so the system stability is easily guaranteed. Furthermore, this controller is available for both small time delays and large time delays. The feasibility and efficiency of the proposed controller are verified through numerical simulations in the end of this paper.     

CHAOTIC MOTIONS AND LIMIT CYCLE FLUTTER OF TWO-DIMENSIONAL WING IN SUPERSONIC FLOW

Based on the piston theory of supersonic flow and the energy method, the flutter motion equations of a two-dimensional wing with cubic stiffness in the pitching direction are established. The aeroelastic system contains both structural and aerodynamic nonlinearities. Hopf bifurcation theory is used to analyze the flutter speed of the system. The effects of system parameters on the flutter speed are studied. The 4th order Runge-Kutta method is used to calculate the stable limit cycle responses and chaotic motions of the aeroelastic system. Results show that the number and the stability of equilibrium points of the system vary with the increase of flow speed. Besides the simple limit cycle response of period 1, there are also period-doubling responses and chaotic motions in the flutter system. The route leading to chaos in the aeroelastic model used here is the period-doubling bifurcation. The chaotic motions in the system occur only when the flow speed is higher than the linear divergent speed and the initial condition is very small. Moreover, the flow speed regions in which the system behaves chaos axe very narrow.