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Detached-eddy simulation of supersonic turbulent flow over rearward facing step
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作者 完颜振海 冯顺山 《Journal of Beijing Institute of Technology》 EI CAS 2011年第3期289-294,共6页
Detailed formulation of the detached-eddy simulation (DES) based on shear stress transport model (SST) was deduced. Based on finite volume method, detached-eddy simulation of super- sonic turbulent flow over rearw... Detailed formulation of the detached-eddy simulation (DES) based on shear stress transport model (SST) was deduced. Based on finite volume method, detached-eddy simulation of super- sonic turbulent flow over rearward facing step was conducted. Multi-block structured non-conform grid was designed. The obtained distribution of wall pressure coefficient along the downstream of the step was in good agreement with experiment. The structure of supersonic flow over rearward facing step is complicated and contains boundary layer-shock interaction, shock-shock interaction and sec- ondary flow separation. The predictions of the corner pressure and location of the reattachment shock are more exact than the Reynolds-averaged method. Results show that detached-eddy simulation can simulate the supersonic separated flows exactly and has advantages over Reynolds-averaged method. The partition of the detached-eddy simulation can be easily achieved by using multi-block non-conform grid, which reduces the requirement of the computational resources as well. 展开更多
关键词 detached-eddy simulation rearward facing step supersonic turbulence SST turbulencemodel
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Universal form of the power spectrum of the aero-optical aberration caused by the supersonic turbulent boundary layer 被引量:1
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作者 高穹 易仕和 姜宗福 《Chinese Physics B》 SCIE EI CAS CSCD 2014年第10期118-123,共6页
Based on the measurement of one-dimensional (1D) optical path difference (OPD) of the supersonic turbulent bound- ary layer, an analytical form for the power spectrum of the two-dimensional (2D) OPD is obtained ... Based on the measurement of one-dimensional (1D) optical path difference (OPD) of the supersonic turbulent bound- ary layer, an analytical form for the power spectrum of the two-dimensional (2D) OPD is obtained with its structure function and under the locally homogeneous isotropic assumption. The universality of this spectrum is argued, and its validity is checked by the comparison with experimental result. The potential applications of this model in theoretical and numerical studies are emphasized. Another contribution of this work is around the application of correlation function to analyzing the statistics of OPD. Based on our results and other results published elsewhere, we show that the OPD is often not stationary, and one should be cautious about using this tool. 展开更多
关键词 AERO-OPTICS supersonic turbulent boundary layer optical path difference power spectrum
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Temporal evolution of the optical path difference of a supersonic turbulent boundary layer 被引量:1
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作者 高穹 易仕和 +2 位作者 姜宗福 何霖 谢文科 《Chinese Physics B》 SCIE EI CAS CSCD 2013年第1期231-236,共6页
The density distribution of a supersonic turbulent boundary layer is measured with the nanoparticle-based planar laser scattering technique, and the temporal evolution of its optical path difference (OPD) in a short... The density distribution of a supersonic turbulent boundary layer is measured with the nanoparticle-based planar laser scattering technique, and the temporal evolution of its optical path difference (OPD) in a short time interval is characterized by proper orthogonal decomposition (POD). Based on the advantage of POD in capturing the energy of a signal, a temporal evolution model is suggested for the POD coefficients of the OPD. In this model, the first few coefficients vary linearly with time, and the others are modeled by Gaussian statistics. As an application, this method is used to compute the shortexposure optical transfer function. 展开更多
关键词 AERO-OPTICS supersonic turbulent boundary layer optical transfer function
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A Hybrid Numerical Simulation of Supersonic IsotropicTurbulence 被引量:1
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作者 Luoqin Liu Jianchun Wang +2 位作者 Yipeng Shi Shiyi Chen X.T.He 《Communications in Computational Physics》 SCIE 2019年第1期189-217,共29页
This paper presents an extension work of the hybrid scheme proposed by Wang et al.[J.Comput.Phys.229(2010)169-180]for numerical simulation of sub-sonic isotropic turbulence to supersonic turbulence regime.The scheme s... This paper presents an extension work of the hybrid scheme proposed by Wang et al.[J.Comput.Phys.229(2010)169-180]for numerical simulation of sub-sonic isotropic turbulence to supersonic turbulence regime.The scheme still utilizes an 8th-order compact scheme with built-in hyperviscosity for smooth regions and a 7th-order WENO scheme for highly compression regions,but now both in their con-servation formulations and for the latter with the Roe type characteristic-wise recon-struction.To enhance the robustness of the WENO scheme without compromising its high-resolution and accuracy,the recursive-order-reduction procedure is adopted,where a new type of reconstruction-failure-detection criterion is constructed from the idea of positivity-preserving.In addition,a new form of cooling function is proposed,which is proved also to be positivity-preserving.With a combination of these techniques,the new scheme not only inherits the good properties of the original one but also extends largely the computable range of turbulent Mach number,which has been further confirmed by numerical results. 展开更多
关键词 supersonic turbulence hybrid scheme positivity-preserving ROR-WENO scheme compact scheme
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超声速流边界层中的壁面正、负压力脉动
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作者 尹琰鑫 吴勇军 +4 位作者 王润 任冲 屈强 张青青 刘晋 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2023年第2期114-125,共12页
本文对来流马赫数2.25、基于动量厚度的雷诺数4000的平板湍流边界层开展了直接数值模拟,通过聚类连通法和条件相关研究了壁面正、负压力脉动.负脉动比正脉动的特征长度小,但是二者特征时间接近.正脉动的对流速度略大.壁面压力脉动结构... 本文对来流马赫数2.25、基于动量厚度的雷诺数4000的平板湍流边界层开展了直接数值模拟,通过聚类连通法和条件相关研究了壁面正、负压力脉动.负脉动比正脉动的特征长度小,但是二者特征时间接近.正脉动的对流速度略大.壁面压力脉动结构的空间距离是自相似的,即空间距离与特征长度成正比.同类壁面压力结构在展向成串出现,正、负壁面压力脉动在流向成对。流向壁面剪切脉动大致在壁面压力脉动的下游,而展向壁面剪切脉动则与壁面压力脉动成对角线方式分布,二者的相关函数成“四极子”形式,其中壁面压力脉动与其上游的展向壁面剪切相关系数大于下游. 展开更多
关键词 supersonic turbulent boundary layer Wall pressure fluctuation Negative and positive events
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吹气比对外凸曲壁湍流再层流化现象的影响
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作者 苏纬仪 张风睿 王谋远 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2022年第5期61-71,I0002,共12页
再层流化是一种边界层加速时湍流向层流或类层流反向转捩的流动现象,它能降低边界层抵抗逆压梯度的能力.为了揭示主动射流方法调控湍流再层流化现象的机理,本文采用大涡模拟方法,研究了不同吹气比对马赫3超声速湍流绕外凸曲壁膨胀加速... 再层流化是一种边界层加速时湍流向层流或类层流反向转捩的流动现象,它能降低边界层抵抗逆压梯度的能力.为了揭示主动射流方法调控湍流再层流化现象的机理,本文采用大涡模拟方法,研究了不同吹气比对马赫3超声速湍流绕外凸曲壁膨胀加速时再层流化现象的影响.结果表明,无控制时,膨胀加速显著降低了大尺度拟序结构和湍动能等湍流特征.施加主动射流控制后,再层流化现象被有效抑制.同时,研究还发现,吹气比在湍流再层流化流动控制中起到重要作用.在相同的射流动量比和静压比条件下,吹气比越大,主动射流抑制再层流化现象的效果越明显. 展开更多
关键词 Relaminarization Air injection supersonic turbulence
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