The dynamic properties of interacting vortex-antivortex pairs in thin film are studied by analytical calculations. An- alytical expressions for the magnetization vector distribution of vortex-antivortex pairs and the ...The dynamic properties of interacting vortex-antivortex pairs in thin film are studied by analytical calculations. An- alytical expressions for the magnetization vector distribution of vortex-antivortex pairs and the trivortex states are given. The magnetic states of the vortices are treated as having rigid structures, i.e., the vortex maintains its spin distribution when moving. The trajectories of the vortex cores are calculated by the Thiele＇s equation. It is found that the vortex-antivortex pair rotates around each other when they have opposite polarities, however, vortex and antivortex cores move along straight lines when they have the same polarity. The frequency of the rotation decreases with increasing the distance between the two cores of vortex-antivortex pair, and it has a lower value when a third vortex is introduced.展开更多
PDF(474KB)Export:BibTeX|EndNote|Reference Manager|ProCite|RefWorks Abstract The one-pion exchange force in addition to the one-gluon exchange force is taken into account to study the mass difference of theπandρmeson...PDF(474KB)Export:BibTeX|EndNote|Reference Manager|ProCite|RefWorks Abstract The one-pion exchange force in addition to the one-gluon exchange force is taken into account to study the mass difference of theπandρmesons with the Bethe–Salpeter equation.After projecting the Bethe–Salpeter equation into a simple form,it can be seen explicitly that the bound energy|Eπ|≫|Eρ|.展开更多
电推进在轨工作时将产生低温稠密等离子体,与地球同步轨道的空间离子体特性存在较大差异,且等离子体中的低速交换电荷离子易受到卫星表面电位的作用,形成返流并作用于卫星表面材料,对航天器表面充放电效应产生重要的影响。为此,综合考...电推进在轨工作时将产生低温稠密等离子体,与地球同步轨道的空间离子体特性存在较大差异,且等离子体中的低速交换电荷离子易受到卫星表面电位的作用,形成返流并作用于卫星表面材料,对航天器表面充放电效应产生重要的影响。为此,综合考虑材料二次电子和背散射电子发射电流,分析电推进产生等离子体充电电流特性,基于充放电平衡方程进行电推进等离子体及空间等离子体共同作用下的表面带电机理研究。研究结果表明:地磁亚暴时期,航天器表面受到地球同步轨道等离子体的影响,其表面电位可高达–10~4 k V;电推进工作时,其羽流等离子体充电电流为10-3 A/m^2,远大于空间等离子体充电电流,从而成为卫星表面带电的主要影响因素;同时电推进等离子体将航天器表面电位中和至–10 V,即电推进交换电荷返流可以有效缓解由空间等离子体造成的危害性表面充放电效应。展开更多
基金Project supported by the National Natural Science Foundation of China(Grant No.11204026)the Fundamental Research Funds for Central Universities of the Ministry of Education of China(Grant No.n130405011)
文摘The dynamic properties of interacting vortex-antivortex pairs in thin film are studied by analytical calculations. An- alytical expressions for the magnetization vector distribution of vortex-antivortex pairs and the trivortex states are given. The magnetic states of the vortices are treated as having rigid structures, i.e., the vortex maintains its spin distribution when moving. The trajectories of the vortex cores are calculated by the Thiele＇s equation. It is found that the vortex-antivortex pair rotates around each other when they have opposite polarities, however, vortex and antivortex cores move along straight lines when they have the same polarity. The frequency of the rotation decreases with increasing the distance between the two cores of vortex-antivortex pair, and it has a lower value when a third vortex is introduced.
基金by National Natural Science Foundation,Grant Number 11075053Program for New Century Excellent Talents in University,Grant Number NCET-07-0282the Fundamental Research Funds for the Central Universities。
文摘PDF(474KB)Export:BibTeX|EndNote|Reference Manager|ProCite|RefWorks Abstract The one-pion exchange force in addition to the one-gluon exchange force is taken into account to study the mass difference of theπandρmesons with the Bethe–Salpeter equation.After projecting the Bethe–Salpeter equation into a simple form,it can be seen explicitly that the bound energy|Eπ|≫|Eρ|.
文摘电推进在轨工作时将产生低温稠密等离子体,与地球同步轨道的空间离子体特性存在较大差异,且等离子体中的低速交换电荷离子易受到卫星表面电位的作用,形成返流并作用于卫星表面材料,对航天器表面充放电效应产生重要的影响。为此,综合考虑材料二次电子和背散射电子发射电流,分析电推进产生等离子体充电电流特性,基于充放电平衡方程进行电推进等离子体及空间等离子体共同作用下的表面带电机理研究。研究结果表明:地磁亚暴时期,航天器表面受到地球同步轨道等离子体的影响,其表面电位可高达–10~4 k V;电推进工作时,其羽流等离子体充电电流为10-3 A/m^2,远大于空间等离子体充电电流,从而成为卫星表面带电的主要影响因素;同时电推进等离子体将航天器表面电位中和至–10 V,即电推进交换电荷返流可以有效缓解由空间等离子体造成的危害性表面充放电效应。
