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Vibrational mode in a two-dimensional dust monolayer is investigated by considering the finite size of dust grains. Each dust grain is assumed to be a negative point charge and a dipole moment due to the inhomogeneous charge distribution on its surface. The dispersion relation of the vibrational mode is derived. Both the self-excited and externally excited cases are discussed. It is shown that the mode is sensitive to the direction of the dipole moment. 相似文献
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介绍单片微型计算实验教学改革的一些做法.自制实验设备,改革实验内容和方法,开放实验室,进行实验考试等.大大地提高了教学质量,增强了学生实验操作能力,科学研究能力和解决问题等方面的能力. 相似文献
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正An academician of Chinese Academy of Sciences (CAS),Professor Changxuan Yu,a long-time professor of plasma physics at the University of Science and Technology of China (USTC),Hefei,China,passed away in Hefei on May 23,2017.Professor Yu was born on July 7,1941,in Java Island,Indonesia,and then moved back to China in 1948 with his parents.He finished his high school 相似文献
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Numerical simulations based on the finite-difference-time-domain (FDTD) approximation to multi-fluid equations for positive ions, negative ions and electrons are used to study high frequency electromagnetic wave propagation and absorption in an unmagnetized plasma layer. The interaction between the incident high frequency wave and the plasma layer shows that the existence of negative ions and the nonlinear effect reduces the power absorption capability of the plasma. Parameter dependences of the effects are calculated and discussed. 相似文献
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强流脉冲离子束(IPIB)及其在靶材中沉积的能量是研究束流与靶材作用的基础.根据三束材料改性国家重点实验室从俄罗斯引进TEMPⅡ型加速器实测的磁绝缘二极管(MID)的加速电压波形及法拉第杯检测到的MID焦点处离子流密度波形,对其进行拟合得到高斯脉冲分布模型,以此为基础采用Monte Carlo方法模拟了离子在铝靶内沉积的能量,得到了一个脉冲内靶材内沉积的能量的时空演化规律.计算了单能离子束以20°~40°角入射铝靶情形.不同能量的单能H+束和C+束以一定角度入射时的最大射程比垂直入射时都要小,表面处单位长度沉积的能量随入射角的增加而增多.IPIB入射铝靶时变化规律同单能离子束.同时对H+和C+二维入射靶材情况也进行了模拟研究. 相似文献
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根据可变体机翼翼表温度检测范围-60~+80℃的要求,提出了一种基于铝板片封装的光纤Bragg光栅(FBG)温度增敏传感装置.该装置采用耐高温环氧树脂胶将FBG粘贴在铝板片U槽中,并预热60℃、保持30 min以保证FBG温度传感增敏装置线性和重复性.研究及试验结果表明,在翼表工作环境温度范围内,该模型理论与实测温度灵敏度分别为28.16 pm/℃和29.03 pm/℃.与裸光栅相比,其增敏倍数分别为2.540倍和2.636倍,增敏倍数误差为3.78%,反射波长与温度的线性度达到0.999 3.因此,在翼体工作环境温度范围内尤其低温环境-60~0℃间,该温度增敏传感装置能满足检测所需精度. 相似文献
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