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An in-depth numerical investigation of a supersonic cavity-ramp flow with DDES method

机译:用DDES方法进行超声腔坡道流的深入数值研究

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Delayed detached eddy simulation (ODES) studies of the highly unsteady supersonic cavity-ramp flow have been successfully carried out. It is generally believed that accurate prediction of the compressible unstable shear layer coupled with the followed reattaching process is a big challenge for ODES method. In the current DDES studies based on an engineering affordable mesh, significant improvements are achieved assessed by the agreements with experimental data. Effects of various crucial parameters related to DOES have been analyzed in detail. First of all, it is found that a fine mesh with sufficient computation domain is required to obtain accurate results, and the time step needs to be properly set. Secondly, effect of the definition of subgrid length scale Delta is observed, especially in the initial region of shear layer. The original Delta form of ODES method tends to depress the development of instabilities in the shear layer. Analysis on the physical causes is presented. Moreover, unexpected performance of ODES' shield function f(d) for the current case is observed and analyzed, whose influence on the simulated characteristic in the downstream region has also been discussed in particular. (C) 2019 Elsevier Masson SAS. All rights reserved.
机译:已经成功地进行了高度不稳定的超音速腔 - 坡道流动的延迟分离涡流模拟(ODES)研究。通常相信,与遵循的重新连接过程相结合的可压缩不稳定剪切层的精确预测是ODES方法的大挑战。在目前基于工程经济实惠的网格的DDES研究中,通过与实验数据的协议评估了显着的改进。已经详细分析了与之相关的各种关键参数的影响。首先,发现具有足够的计算域的精细网格需要获得准确的结果,并且需要正确设置时间步长。其次,观察到底图长度Δdδ的定义的效果,尤其是在剪切层的初始区域中。原始的杂散方法方法倾向于抑制剪切层中稳定性的发展。提出了对物理原因的分析。此外,观察并分析了用于当前情况的ODES屏蔽功能F(D)的意外性,其对下游区域中的模拟特性的影响也尤其讨论。 (c)2019年Elsevier Masson SAS。版权所有。

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