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arXiv 1709.01302cond-mat.mes-hall
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自旋-轨道力矩中的牛顿第二定律

Newton's second law in spin-orbit torque

Cong Son Ho, Seng Ghee Tan, Shun-Qing Shen, Mansoor B. A. Jalil

摘要:

自旋-轨道力矩(SOT)是指在施加带电电流的情况下经由自旋-轨道耦合的磁化动力学的激发。在这项工作中,我们介绍了一个简单而直观的描述的SOT的自旋力。在Rashba自旋轨道耦合系统中,类阻尼的SOT可以表示为${\mathbf T}^\mathrm{so}={\mathbf R}_c\times {\mathbf F}^{\mathrm {so}}$,类似于经典的力矩-力关系,其中$R_c$是动量空间中表征Rashba分裂的有效半径.因此,磁能被转移到传导电子,传导电子以$({\mathbf j}_e\cdot {\mathbf F}^{\mathrm {so}})$的速率通过焦耳加热耗散,其中$j_e$是施加的电流。最后,我们提出了一个实验验证我们的研究结果,通过测量的各向异性磁阻效应。

英文摘要:

Spin-orbit torque (SOT) refers to the excitation of magnetization dynamics via spin-orbit coupling under the application of a charged current. In this work, we introduce a simple and intuitive description of the SOT in terms of spin force. In Rashba spin-orbit coupling system, the damping-like SOT can be expressed as ${\mathbf T}^\mathrm{so}={\mathbf R}_c\times {\mathbf F}^{\mathrm {so}}$, in analogy to the classical torque-force relation, where $R_c$ is the effective radius characterizing the Rashba splitting in the momentum space. As a consequence, the magnetic energy is transferred to the conduction electrons, which dissipates through Joule heating at a rate of $({\mathbf j}_e\cdot {\mathbf F}^{\mathrm {so}})$, with $j_e$ being the applied current. Finally, we propose an experimental verification of our findings via measurement of the anisotropic magnetoresistance effect.

机构、总结、中文摘要均由AI分析而来,可能存在错误,请以论文正文为准。

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