一种模拟动边界绕流的锐利界面浸入边界法

When the structural wall moves over a fixed grid, the structure coverage will change, resulting in many dead and emerging elements. To avoid the influence of malformation and reconstruction of body-fitted grids on the calculation efficiency and accuracy of the fluid-structure interaction problems with coupled boundary movement on the fixed grid, an improved numerical method for describing the interaction between an immersed rigid body and fluid based on a sharp-interface is proposed. In this method, both the fluid and solid are regarded as pure fluid domains in the whole computational domain, and the solid boundary is divided into several Lagrangian grid points. The flow parameter or velocity is reconstructed by interpolation at the interface element, which is then directly used as the boundary condition of the flow field, thus reflecting the influence of the wall boundary conditions. The method constructs the calculation structure of “virtual point, force point and vertical foot point”, and the velocity of the virtual point is obtained by bilinear interpolation. Then, the velocity of the force point is calculated by forcing the solid boundary to meet the no-slip condition, and the equations of the coupling system based on the immersion boundary method are finally solved to realize the numerical simulation of the flow with a complex moving boundary. The numerical program for this immersed boundary method is established using C++, then the accuracy and reliability of the proposed method are validated by comparison with the literature and experimental results of the basic numerical example of flow around a cylinder. Furthermore, the effects of the structural shape and the angle of attack on the trailing vortex structure, the vortex shedding frequency, and the lift/ coefficient characteristics of the flow around the elliptical cylinder have been analyzed. The anti-symmetric S-type, “P+S” Ⅰ-type and “P+S” Ⅱ-type trailing vortex shedding modes, as well as the variation laws of the vortex structure size, vortex shedding frequency and lift-drag coefficients ratio with axis ratio and angle of attack, are captured. The critical angle of attack (25°) corresponding to the maximum lift-drag ratio is determined as 25°.     

椭圆柱电缆单位长度的自感计算

利用复数坐标系z上的儒可夫斯基变换,计算长直椭圆柱电缆单位长度的自感,并对结果进行讨论.     

高速气体与椭圆柱云相互作用的数值研究

高速颗粒流在天文、自然灾害、工业安全、医疗工业和国防等领域有着重要应用。采用基于分层流模型的直接数值模拟方法,对平面激波与椭圆柱云的相互作用进行数值研究,重点关注椭圆柱横截面的不同长短轴之比和椭圆柱横截面长轴与来流方向所成角度对流场的影响,从气体来流方向上的速度、x轴和y轴方向上的均方根速度、动能、内能和湍动能的分布上进行分析,对能量在计算域的上游区域、椭圆柱云区域和下游区域进行定量分析。同时针对椭圆柱改进了一维体积平均模型,利用该模型拟合了由直接数值模拟得到的反射激波和透射激波位置,获得了最适配的一维体积平均模型中的人工有效阻力系数,并探讨此系数的分布规律。     

线电荷与带有半椭圆柱凸起的接地平板系统的电势

利用儒可夫斯基变换,求解线电荷与带有半椭圆柱凸起的接地平板导体的电势分布,并用Matlab软件绘出电势分布图.     

椭圆柱壳链的波形弥散特性研究

椭圆柱壳链可以引起波形弥散，从而可以调控应力波的传播.本文通过3D打印、冲击测试、细观有限元模拟和理论分析，研究了在质量块冲击加载下，单胞纵横比、冲击质量和速度对椭圆柱壳链中弹性波传播弥散行为的影响.结果表明，冲击过程中，椭圆柱壳链结构中的速度峰值随着波传播逐渐减小，纵横比越大或冲击质量越小，速度峰值衰减越剧烈，而冲击速度对椭圆柱壳链的波形弥散行为几乎无影响.相关研究对新型波形控制器的设计和精确有效地调控弹性波传播具有重要意义.     

共焦椭圆导体柱板间的电场分布

根据椭圆柱板间的等势线方程,利用解析函数的性质,导出了共焦椭圆柱板间的电场分布.     

用儒可夫斯基变换计算椭圆柱螺线管的磁场

利用复数坐标系z平面上的儒可夫斯基变换,计算长直椭圆柱螺线管的磁场．     

用高斯定理解题的可解性条件

给出应用高斯定理由直接积分法求解静电场问题时的可解性条件,用反例说明常见教科书中对此问题的表述是不完备的.     

超音速后掠椭圆柱横流定常涡的不稳定特性及转捩预测

实验发现,一定条件下超声速后掠圆柱的前半圆上可能发生定常涡引起的转捩.为了模拟高空超音速飞行器后掠翼前缘,以无限展向长度后掠椭圆柱为模型,基于eN方法,根据积分的N值,分析了迎风轴长度、Reynolds(雷诺)数、后掠角和Mach(马赫)数等参数的变化对超音速后掠椭圆柱横流定常涡不稳定性的影响.研究结果表明,后掠椭圆柱的迎风轴长度增加,会使横流定常涡的不稳定性增强;Reynolds数增大,使横流定常涡模态的不稳定性增强;不稳定性的强度与Reynolds数的大小为近似线性关系;飞行高度增加,Mach数变大,使横流定常涡的不稳定性变弱;后掠角在一定范围内的变化对横流定常涡的不稳定性影响不大.这些结果有助于提高对高空超音速飞行器翼前缘转捩机理的认识,为横流转捩预测提供理论指导