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圆偏振光的后向散射旋性反转特性分析 被引量:3
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作者 于洋 范之国 +1 位作者 徐少罕 高隽 《中国激光》 EI CAS CSCD 北大核心 2015年第11期213-221,共9页
圆偏振光较线偏振光具有更多的潜在优势,尤其是在浑浊介质中,利用圆偏振光的旋性进行目标探测可以有效抑制散射光的影响。从经典单粒子偏振态描述方法出发,从散射介质属性和单次散射角大小的角度,阐明了圆偏振光在散射介质中旋性反转与... 圆偏振光较线偏振光具有更多的潜在优势,尤其是在浑浊介质中,利用圆偏振光的旋性进行目标探测可以有效抑制散射光的影响。从经典单粒子偏振态描述方法出发,从散射介质属性和单次散射角大小的角度,阐明了圆偏振光在散射介质中旋性反转与保持的机理,并通过蒙特卡罗方法建模仿真,分析了圆偏振光的后向散射旋性反转特性。仿真结果表明,单次散射后,圆偏振光旋性的保持或反转取决于散射介质的属性及散射角的大小;多次散射后,圆偏振光的旋性保持或反转还和光子入射方向与光子接收面夹角的大小相关。特别地,圆偏振光的后向散射在低浓度散射介质中或短距离传输时会发生旋性反转,而在浑浊介质即高浓度散射介质中或远距离传输时会保持其初始偏振态。 展开更多
关键词 大气光学 圆偏振光 后向散射 蒙特卡罗方法 旋性反转
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切边纳米铁磁盘对中磁涡旋旋性的磁场调控 被引量:1
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作者 马晓萍 杨宏国 +2 位作者 李昌锋 刘有继 朴红光 《物理学报》 SCIE EI CAS CSCD 北大核心 2021年第10期289-295,共7页
铁磁纳米盘中的磁涡旋态因稳定性高,并且其面内磁化的旋转方向具有天然的二向性(顺时针(CW)和逆时针(CCW)),可以作为信息存储的一个比特单元而成为最近研究的热点.基于磁涡旋旋性的信息存储要求人们能够独立地控制磁涡旋的旋转方向.从... 铁磁纳米盘中的磁涡旋态因稳定性高,并且其面内磁化的旋转方向具有天然的二向性(顺时针(CW)和逆时针(CCW)),可以作为信息存储的一个比特单元而成为最近研究的热点.基于磁涡旋旋性的信息存储要求人们能够独立地控制磁涡旋的旋转方向.从旋性的角度考虑,在一对纳米盘中可能出现四种磁涡旋基态,即(CCW,CCW),(CCW,CW),(CW,CCW)和(CW,CW).本文通过引入厚度不同且切边的纳米磁盘对,并对其施加面内磁场来实现对四种涡旋基态的独立控制,并通过微磁学模拟证明了这种方法的可行性. 展开更多
关键词 磁涡 旋性反转 纳米磁盘 微磁学模拟
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Unusual Charge Transport and Spin Response of Doped Bilayer Triangular Antiferromagnets 被引量:3
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作者 LIANGying MATian-Xing FENGShi-Ping 《Communications in Theoretical Physics》 SCIE CAS CSCD 2003年第6期749-756,共8页
Within the t-J model, the charge transport and spin response of the doped bilayer triangular antiferromagnetare studied by considering the bilayer interaction. Although the bilayer interaction leads to the band splitt... Within the t-J model, the charge transport and spin response of the doped bilayer triangular antiferromagnetare studied by considering the bilayer interaction. Although the bilayer interaction leads to the band splitting in theelectronic structure, the qualitative behaviors of the physical properties are the same as in the single layer case. Theconductivity spectrum shows the low-energy peak and unusual midinfrared band, the temperature-dependent resistivityis characterized by the nonlinearity metallic-like behavior in the higher temperature range and the deviation from themetallic-like behavior in the lower temperature range and the commensurate neutron scattering peak near the half-fillingis split into six incommensurate peaks in the underdoped regime, with the incommensurability increasing with the holeconcentration at lower dopings, and saturating at higher dopings. 展开更多
关键词 charge transport spin response t-J model
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Mass transfer characteristics in a rotating packed bed with split packing 被引量:4
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作者 Youzhi Liu Deyin Gu +2 位作者 Chengcheng Xu Guisheng Qi Weizhou Jiao 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2015年第5期868-872,共5页
The rotating packed bed (RPB) with split packing is a novel gas-liquid contactor, which intensifies the mass transfer processes controlled by gas-side resistance. To assess its efficacy, the mass transfer characteri... The rotating packed bed (RPB) with split packing is a novel gas-liquid contactor, which intensifies the mass transfer processes controlled by gas-side resistance. To assess its efficacy, the mass transfer characteristics with adjacent rings in counter-rotation and co-rotation modes in a split packing RPB were studied experimentally. The physical absorption system NH3-H2O was used for characterizing the gas volumetric mass transfer coeffi- cient (kyae) and the effective inteffacial area (ae) was determined by chemical absorption in the CO2-NaOH sys- tem. The variation in kyae and ae with the operating conditions is also investigated. The experimental results indicated that kyae and ae for counter-rotation of the adjacent packing rings in the split packing RPB were higher than those for co-rotation, and both counter-rotation and co-rotation of the split packing RPB were superior over conventional RPBs under the similar ooerating conditions. 展开更多
关键词 Rotating packed bed (RPB) Split packing Mass transfer Physical absorption Chemical absorption
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Influence of exit-to-throat width ratio on performance of high pressure convergent-divergent rotor in a vaneless counter-rotating turbine 被引量:3
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作者 ZHANG Lei WANG HuiShe +1 位作者 LUO WeiWei XU JianZhong 《Science China(Technological Sciences)》 SCIE EI CAS 2011年第3期723-732,共10页
This paper describes the redesign of a high pressure rotor (with exit Mach number around 1.5) for the vaneless counter-rotating turbine by choosing adequate exit-to-throat width ratio. Based on the previous design ana... This paper describes the redesign of a high pressure rotor (with exit Mach number around 1.5) for the vaneless counter-rotating turbine by choosing adequate exit-to-throat width ratio. Based on the previous design analysis and test results, effects of the exit-to-throat width ratio on the performance of the transonic turbine cascade were proposed. In order to investigate the influence of the exit-to-throat width ratio on the performance of the turbine cascade, a flow model of the convergent-divergent turbine cascade was constructed by using the theory of Laval nozzle. Then a method on how to choose the adequate exit-to-throat width ratio for the turbine cascade was proposed. To validate the method, it was used to calculate the adequate exit-to-throat width ratio for the high pressure rotor of the vaneless counter-rotating turbine. The high pressure turbine rotor was redesigned with the new exit-to-throat width ratio. Numerical simulation results show that the isentropic efficiency of the redesigned vaneless counter-rotating turbine under the design condition has increased by 0.9% and the efficiencies under the off-design conditions are also improved significantly. On the original design, a group of compressional waves are created from the suction surface after about 60% axial chord in the high pressure turbine rotor. While on the new design the compressional waves are eliminated. Furthermore, on the original design, the inner-extending waves first impinge on the next high pressure turbine rotor suction surface. Its reflection is strong enough and cannot be neglected. However on the new design the inner-extending waves are weakened or even eliminated. Another main progress is that the redesigned high pressure turbine rotor is of practical significance. In the original rotor, a part of the blade (from 60% axial chord to the trailing edge) is thin leading to the intensity problem and difficult arrangement of the cooling system. In the new design, however, the thickness distribution of the rotor airfoil along the chord is relatively reasonable. The intensity of the rotor is enhanced. It is possible to arrange the cooling system reasonably. 展开更多
关键词 exit-to-throat width ratio counter-rotating turbine transonic turbine high pressure rotor
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