Thermal and Electrical Conductivities of a Three-Dimensional Ideal Anyon Gas with Fractional Exclusion Statistics

The thermal and electrical transport properties of an ideal anyon gas within fractional exclusion statistics are studied. By solving the Boltzmann equation with the relaxation-time approximation, the analytical expressions for the thermal and electrical conductivities of a three-dimensional ideal anyon gas are given. The low-temperature expressions for the two conductivities are obtained by using the Sommerfeld expansion. It is found that the Wiedemann–Franz law should be modified by the higher-order temperature terms, which depend on the statistical parameter g for a charged anyon gas. Neglecting the higher-order terms of temperature, the Wiedemann–Franz law is respected, which gives the Lorenz number. The Lorenz number is a function of the statistical parameter g.     

Two Ni~Ⅱ/Cu~Ⅱ Coordination Polymers Based on Pyridyl-carboxylate Ligand: Synthesis,Crystal Structures and Magnetic Properties

Under hydrothermal conditions, the reactions of Ni~Ⅱ/Cu~Ⅱ ions with 3-(6-aminpyridinium-3-yl) benzoate(HL) afford two compounds [NiL 2]n(1) and [Cu L2(H2 O)]n(2). On the basis of X-ray diffraction analysis of the two compounds, the results show that compound 1 features one-dimensional(1 D) double-strand coordination arrays, while 2 presents the 63-hcb layers. Both compounds are further constructed into a 3 D supramolecular structure with the aid of weak secondary interactions. Thermal stabilities and magnetic properties of compounds 1 and 2 were also investigated.     

BCS-BEC渡越过程超流费米气体在线性变化势中的集体激发

基于超流流体力学方程组和标度理论,数值研究了Bardeen-Cooper-Schrieffer (BCS)-Bose-Einstein Condensate (BEC)渡越过程中超流费米气体在线性减小谐振子势下的集体激发.详细研究了包括谐振子势频率线性减小的速度,减小到的幅度以及势阱各向异性参数对集体激发的影响.通过频谱分析和数据拟合,分别研究了各向同性势和各向异性势下在最小振幅激发下所对应的模式,且数值计算得到的频率值在整个BCS-BEC渡越过程中与前期的理论结果符合得很好.该工作可以为后面超流费米气体集体激发的实验提供有益的理论参考     

基于非线性耦合本构关系模型的尖化前缘气动加热影响研究

结合数值模拟与风洞试验技术,在高超声速连续/稀薄滑移流条件下对尖化前缘这一典型构型的气动加热影响开展深入研究.在三维有限体积框架下,应用非线性耦合本构关系(nonlinear coupled constitutive relations, NCCR)模型对试验工况下的尖化前缘外形开展数值计算,检验NCCR模型在尖化前缘构型中准确描述局部稀薄非平衡流动和物面气动热的性能.数值结果与实验数据对比表明,在等效高度33 km的风洞试验条件下, NCCR模型计算得到的驻点热流系数峰值同实验值偏差为1.81%, Fay-Riddell公式和纳维-斯托克斯(Navier-Stokes, NS)方程得到的驻点热流系数峰值同实验值偏差均在5%以内,物面其他位置的壁面热流系数计算值与实验值偏差均在10%以内,证明此时飞行器尖化前缘区域局部稀薄气体效应对气动加热影响程度较弱;在等效高度60 km时,飞行器尖化前缘区域附近的局部稀薄气体效应对气动加热的影响较为明显, NS方程计算的驻点热流系数偏差为33.31%, Fay-Riddell公式计算驻点热流系数同实验值偏差为29.5%, NCCR模型计算的驻点热流...