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Direct numerical simulation of spatially developing highly compressible mixing layer: Structural evolution and turbulent statistics

机译:空间开发高度可压缩混合层的直接数值模拟:结构演化与湍流统计

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摘要

Direct numerical simulation of a spatially developing supersonic mixing layer with a convective Mach number of 1.0 is conducted. The present work focuses on the structural evolution and the turbulent statistics, and both instantaneous and time-averaged data are utilized to obtain further insight into the dynamical behaviors of the flow. The full development process of instability, including the shear action at the flow early stage, the generation of kinds of typical vortex structures in the flow transition region, and the establishment of self-similar turbulence, is clearly presented. The formation and evolution mechanisms of multiple ring-like vortices are reported and analyzed using the Helmholtz first law in compressible mixing layers, and the role they play in the mixing process in the flow transition stage is researched. The mean velocity distribution and the turbulent intensities are found to have close relations with the evolution of the multiple ring-like vortices. The presence of multiple ring-like vortices leads to local strong ejection and sweep regions that create pockets of partially mixed fluid near the tips of the vortices, which contributes much to the huge energy and momentum transfer of the upper and lower streams. Some anisotropy coefficients and turbulent structure parameters are described and analyzed to better reveal the effects of multiple ring-like vortices on flow behaviors. Our results indicate that with the increase in compressibility, though in a fully turbulent region, mixing layer growth and turbulent intensities are both suppressed, the appearance of multiple ring-like vortices and their evolutions can significantly promote mixing in the transition stage, which is usually ignored by previous researchers. Therefore, employing flow control methods to extend the flow transition stage and help sustain multiple ring-like vortices over a longer distance is a possible technique to enhance mixing. Published under license by AIP Publishing
机译:进行具有对流马赫数为1.0的空间发展超音速混合层的直接数值模拟。目前的工作侧重于结构演变和湍流统计,并且瞬时和时间平均数据都利用了进一步了解流量的动态行为。清楚地呈现了不稳定性的完整开发过程,包括流程早期的剪切动作,流过渡区域中的典型涡流结构以及自相似湍流的建立。报告了多个环状涡旋的形成和演化机制,并使用Helmholtz第一法在可压缩混合层中进行分析,并研究了流动过渡阶段混合过程中的作用。发现平均速度分布和湍流强度与多环样涡流的演变具有密切的关系。多个环状涡流的存在导致局部强弹性和扫掠区域,其产生部分混合的流体袋,扭转涡流的尖端,这有助于上部和下部流的巨大能量和动量转移。描述并分析了一些各向异性系数和湍流结构参数,以更好地揭示多个环状涡流对流动行为的影响。我们的结果表明,随着可压缩性的增加,尽管在完全湍流区域,混合层生长和湍流强度都被抑制,但多个环状涡流的外观和它们的演进可以显着促进过渡阶段的混合,这通常是以前的研究人员忽略了。因此,采用流量控制方法延长流动过渡阶段,并帮助在更长的距离上维持多个环状涡流,是增强混合的可能技术。通过AIP发布在许可证下发布

著录项

  • 来源
    《Physics of fluids》 |2019年第3期|共20页
  • 作者单位

    Natl Univ Def Technol Sci &

    Technol Scramjet Lab Changsha 410073 Hunan Peoples R China;

    Natl Univ Def Technol Sci &

    Technol Scramjet Lab Changsha 410073 Hunan Peoples R China;

    Natl Univ Def Technol Sci &

    Technol Scramjet Lab Changsha 410073 Hunan Peoples R China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 流体力学;
  • 关键词

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