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首页> 外文期刊>Mathematical Problems in Engineering >Curvilinear Coordinate System for Mathematical Analysis of Inclined Buoyant Jets Using the Integral Method
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Curvilinear Coordinate System for Mathematical Analysis of Inclined Buoyant Jets Using the Integral Method

机译:积分法求解斜浮力射流的曲线坐标系

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The development of a local system of orthogonal curvilinear coordinates, which is appropriate to monitor the flow of an inclined buoyant jet with reference to the basic Cartesian coordinate system is presented. Such a system is necessary for the correct application of the integral method, since the well-known Gaussian profiles should be integrated on the cross-sectional area of inclined buoyant jet, where they are valid. This is the major advantage of the present work compared to all other integral methods using Cartesian coordinate systems. Consequently, the flow and mixing governing partial differential equations (PDE), i.e., continuity, momentum, buoyancy, and/or tracer conservation, are written in the local orthogonal curvilinear coordinate system and, then, the Reynolds substitution regarding mean and fluctuating components of all dependent variables is applied. After averaging with respect to time, the mean flow PDEs are taken, omitting second-order terms, as the dynamic pressure and molecular viscosity, compared to the mean flow and mixing contributions of turbulent terms. The latter are introduced through empirical coefficients. The Boussinesq's approximation regarding small density differences is taken into consideration. The system of PDEs is closed by assuming known spreading coefficients along with Gaussian similarity profiles. The methodology is applied in the inclined two-dimensional buoyant jet; thus, PDEs are integrated on the jet cross-sectional area resulting in ordinary differential equations (ODE), which are appropriate to be solved by applying the 4th order Runge-Kutta algorithm coded in either FORTRAN or EXCEL. The numerical solution of ODES, concerning trajectory of the inclined two-dimensional buoyant jet, as well as longitudinal variations of the mean axial velocity, mean concentration, minimum dilution, and entrainment velocity or entrainment coefficient, occurs quickly, saving computer memory and effort. The satisfactory agreement of results with experimental data available in the literature empowers the usefulness of the proposed methodology in inclined buoyant jets.
机译:提出了正交曲线坐标的局部系统的开发,该系统适用于参考基本笛卡尔坐标系来监视倾斜的浮力射流。这样的系统对于正确应用积分方法必不可少,因为众所周知的高斯轮廓应该在有效的倾斜浮力射流的横截面上集成。与使用笛卡尔坐标系的所有其他积分方法相比,这是当前工作的主要优点。因此,控制局部偏微分方程(PDE)的流动和混合,即连续性,动量,浮力和/或示踪剂守恒,被写在局部正交曲线坐标系中,然后,用雷诺兹代入法关于均值和波动分量应用所有因变量。在对时间进行平均后,取平均流量PDE,与湍流术语的平均流量和混合贡献相比,将二阶项作为动态压力和分子粘度予以忽略。后者是通过经验系数引入的。考虑到关于小密度差的Boussinesq近似。通过假设已知的扩展系数以及高斯相似性曲线来封闭PDE系统。该方法应用于倾斜的二维浮力射流。因此,PDE被集成在射流横截面上,从而产生常微分方程(ODE),适用于应用以FORTRAN或EXCEL编码的四阶Runge-Kutta算法来求解。关于倾斜二维浮力射流的轨迹以及平均轴向速度,平均浓度,最小稀释度和夹带速度或夹带系数的纵向变化,ODES的数值解决方案可以快速出现,从而节省了计算机内存和精力。结果与文献中可用的实验数据的令人满意的一致性使所提出的方法在倾斜浮力射流中的有用性。

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