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Numerical simulation of propagation of plane turbulent straitened jet in counter flow using LES turbulence model

机译:使用LES湍流模型在逆流中平面湍流划线射流传播的数值模拟

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In technical applications are often used jets, emerging in the counter. Experimental study of such flows for the plane and axisymmetric cases was carried out in [1-5]. In [4] with an approximate integral method and some hypotheses about the nature of the course, based on experimental data obtained approximate analytical expressions for the basic characteristics of axisymmetric flow within the boundary layer for the case of a1, where a-geometric parameter characterizing the ratio of the size of the incoming flow and the jet directed toward him. In experimental studies also generally considered the case of large values of a. The following research carried out for the plane case for moderate values of a =10÷25, in which the essential straitness jet. Calculations were carried out on the basis of time-dependent system of Navier-Stokes equations for turbulent flow, implemented using LES turbulence model in the complex ANSYS CFX. On the basis of the conservation laws for an analytical assessment of the range of parameters in which there is a solution to the problem, and compared the results of the numerical solution with the available experimental data.
机译:在技​​术应用中,通常使用喷气机,在计数器中出现。对平面和轴对称壳体流动的实验研究进行了[1-5]。在[4]的近似积分法和有关过程的性质,基于实验数据一些假设得到的近似解析表达式对轴对称流动的基本特征的边界层内,用于的 1的情况,其中的α-几何参数表征传入流量的尺寸和向他指向的喷射器的比率。在实验研究中,通常也认为大量值的情况。以下研究对平面壳体的平面案例进行了适用于A = 10°25的中等值,其中必要的穴位喷射。在湍流的湍流中基于湍流的时间依赖性系统进行计算,在复杂的Ansys CFX中使用LES湍流模型实现。在守恒法的基础上,分析评估存在问题的参数范围,并将数值解决方案的结果与可用的实验数据进行比较。

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