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Josephson结的I-V曲线的子台阶 被引量:1
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作者 刘曾荣 江霞妹 +1 位作者 韩志斌 顾国庆 《物理学报》 SCIE EI CAS CSCD 北大核心 1990年第5期823-829,共7页
本文在文献[1]基础上进一步分析Josephson结的I-V曲线的子台阶现象。首先把数学方法作了发展,然后用所得的方法分析了产生子台阶的条件,从而完善了对Josephson结的I-V曲线的分析。
关键词 JOSEPHSON结 I-V曲线 子台阶
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含约瑟夫森结电路的特性分析和研究 被引量:1
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作者 王玲 郑善贤 《微电子学》 CAS CSCD 北大核心 2003年第3期218-220,共3页
 提出了超导约瑟夫森结模型(并联电阻-电容结模型),给出了约瑟夫森效应的一些重要结果。在分析约瑟夫森结电路方程时,研究了其中出现的混沌特性和子台阶现象。计算获得的结果对混沌数字通信和超导电子学的应用将起到重要作用。
关键词 约瑟夫森结电路 约瑟夫森效应 子台阶现象 超导电 隧道结 混沦动力学 超导材料
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Marked Advance in Widths and Heights of Harmonic Plateau
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作者 陈高 朱颀人 《Communications in Theoretical Physics》 SCIE CAS CSCD 2010年第4期759-763,共5页
We propose a scheme to simultaneously widen and heighten the high-order harmonic plateau on a large scale. More specifically, by adopting a united two-atom system with a suitable inter-nuclear separation instead of a ... We propose a scheme to simultaneously widen and heighten the high-order harmonic plateau on a large scale. More specifically, by adopting a united two-atom system with a suitable inter-nuclear separation instead of a single-atom, the harmonic plateau is widened from Ip + 3.2Up to Ip +8.5Up; further, by adopting the combined pulse, the extended plateau (harmonics near Ip+ 5.6Up) is selectively heightened in excess of 4 orders of magnitude compared with the case of the low-frequency pulse alone. By means of the wavelet transform for the induced dipole of these harmonics, a single x-ray pulse as short as 210 asec is achieved. 展开更多
关键词 high-order harmonic generation united two-atom model combined pulse
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Three Dimensional Numerical Analysis of Flow within an Isolated Rotor with Stepped Blades 被引量:1
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作者 Shervin Sammak Masoud Boroomand 《Journal of Thermal Science》 SCIE EI CAS CSCD 2012年第5期420-427,共8页
Every compressor works in a limited operational range. Surge as one of the sources of this limitation has been studied for many years. In this research, an isolated blade row of compressor rotor is numerically modeled... Every compressor works in a limited operational range. Surge as one of the sources of this limitation has been studied for many years. In this research, an isolated blade row of compressor rotor is numerically modeled and solved. In order to improve operational limit and postpone the surge occurrence, a stepped blade of RAF6E with higher stall angle of attack is used to investigate the near stall flow behavior. In this study, several location of step on blades are tried and the results are compared with the case with no step on blades. It is shown that, as the step moves toward the leading edge of blades, the effect of delay on surge is reduced and even efficiency is also decreased significantly. By moving the step towards the trailing edge, surge is delayed due to the reattachment of flow after the step. Efficiency is also decreased but not in the order of the previous case. 展开更多
关键词 compressor performance efficiency stable operational margin stepped airfoil surge improvement
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