Analysis of influencing factors on numerical simulation of transverse jet in supersonic flow

Jiang-Fei Yu, Tao Tang, Jin-cheng Zhang, Da-Peng Xiong, Hong-Bo Wang, Ming-Bo Sun
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Abstract

Numerical simulation is becoming an important research method in the field of supersonic flow. Its accuracy and reliability have always been the key to its further application and the focus of current researches. In this study, a series of numerical simulations of transverse supersonic jet in supersonic free flow are carried out based on Reynolds averaged (RANS) solver. Firstly, the flow field structure obtained by different calculation cases is studied, and the mechanism of the difference of flow field structure is described. Furthermore, by changing the accuracy of difference scheme for the convection term and the turbulence model, the different simulation results are compared with the experimental data. The deviation from numerical simulation compared with the experiment is further analyzed to clarify the critical factors affecting the calculation reliability. The results show that improving the accuracy of the scheme cannot effectively improve the calculation results, while choosing an appropriate turbulence model can be helpful to improve the calculation accuracy. When the numerical simulation of jet flow mixing in supersonic flow field is carried out, the conclusions of this study can provide a support for determining the numerical model method and error analysis.
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超音速流中横向射流数值模拟的影响因素分析
数值模拟正在成为超音速流动领域的一种重要研究方法。其准确性和可靠性一直是其进一步应用的关键,也是当前研究的重点。本研究基于雷诺平均(RANS)求解器,对超音速自由流中的横向超音速射流进行了一系列数值模拟。首先,研究了不同计算情况下得到的流场结构,并描述了流场结构差异的机理。此外,通过改变对流项和湍流模型的差分方案精度,将不同的模拟结果与实验数据进行了比较。进一步分析了数值模拟与实验结果的偏差,以明确影响计算可靠性的关键因素。结果表明,提高方案精度并不能有效改善计算结果,而选择合适的湍流模型则有助于提高计算精度。在进行超音速流场射流混合数值模拟时,本研究的结论可为确定数值模型方法和误差分析提供支持。
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