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On the use of Boussinesq approximation in turbulent supersonic jet modeling

机译:关于Boussinesq逼近在湍流超音速射流建模中的应用

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摘要

The problem of turbulent supersonic jet modeling within the limits of Reynolds-averaged Navier-Stokes equations and Boussinesq approximation was considered. The time-asymptotic technique for full Navier-Stokes equations and the space-marching technique for parabolized Navier-Stokes equations were used to solve this problem. A variety of turbulence models was applied in an effort to obtain a good consistency with the experimental data on two distinct features of non-isobaric jets, namely, the mean flow decay and the shock wave attenuation. It was revealed that the Boussinesq approximation in its general form used in the full Navier-Stokes equations fails to reproduce these two features together. As regards the parabolized Navier-Stokes equations, such an abbreviated form gets practically rid of this failure. A solid theoretical interpretation of this effect was found, whereupon new forms of the turbulent viscosity terms were proposed and analyzed. It was ascertained that they offer considerable advantages over the Boussinesq approximation in some CFD applications.
机译:考虑了在雷诺平均Navier-Stokes方程和Boussinesq逼近范围内的湍流超音速射流建模问题。完整的Navier-Stokes方程的时间渐近技术和抛物线化Navier-Stokes方程的空间行进技术用于解决此问题。为了在非等压射流的两个不同特征(即平均流量衰减和冲击波衰减)上获得与实验数据的良好一致性,应用了各种湍流模型。结果表明,在完整的Navier-Stokes方程中使用的一般形式的Boussinesq逼近无法将两个特征一起重现。关于抛物线型的Navier-Stokes方程,这种缩写形式实际上消除了这种失败。找到了对此效应的可靠理论解释,随后提出并分析了新形式的湍流粘度项。可以确定的是,在某些CFD应用中,它们比Boussinesq近似具有明显的优势。

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