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Mixing characteristics of a transverse jet injection into supersonic crossflows through an expansion wall

机译:横向喷流通过扩展壁注入超声速横流的混合特性

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摘要

Mixing characteristics of a transverse jet injection into supersonic crossflows through an expansion plate are investigated using large eddy simulation (LES), where the expansion effects on the mixing are analyzed emphatically by comparing to the flat-plate counterpart. An adaptive central-upwind weighted essentially non oscillatory (WENO) scheme along with multi-threaded and multi-process MPI/OpenMP parallel is adopted to improve the accuracy and efficiency of the calculations. Progressive mesh refinement study is performed to assess the grid resolution and solution convergence. Statistic results obtained are compared to the experimental data and recently performed classical numerical simulation, which validates the reliability of the present LES codes. Firstly, the jet mixing mechanisms in the flowfield with expansion plate are revealed. It indicates that the large-scale vortices in the windward side of jet plume induced by Kelvin-Helmholtz (K-H) instability contribute to the mixing in the near-field, while the entrainment by the counter-rotating vortices and molecular diffusion dominate the mixing process in the far-field. Furthermore, the effects of wall expansion on the flow and mixing characteristics are discussed. The boundary layer across the expansion corner is relaminarized and the profiles of streamwise velocity are distinctly changed. Then the separation region ahead of jet plume is more close to the wall, and the breaking process of large-scale vortices in the windward side of jet plume starts earlier. However, the favorable pressure gradient generated by wall expansion reduces the mixing efficiency and brings a greater total pressure loss.
机译:使用大涡模拟(LES)研究了通过膨胀板向超声速横流中注入横向射流的混合特性,并通过与平板对应物进行对比,着重分析了混合时的膨胀效应。采用自适应中央逆风加权基本非振荡(WENO)方案以及多线程和多进程MPI / OpenMP并行,以提高计算的准确性和效率。进行渐进式网格细化研究以评估网格分辨率和解收敛性。将获得的统计结果与实验数据进行比较,并且最近进行了经典的数值模拟,从而验证了当前LES代码的可靠性。首先,揭示了带有扩展板的流场中的射流混合机理。这表明由开尔文-亥姆霍兹(KH)不稳定性引起的射流羽状迎风侧的大涡旋有助于近场的混合,而反向旋转涡旋的夹带和分子扩散则主导了混合过程。在远场。此外,讨论了壁膨胀对流动和混合特性的影响。重新扩展了扩展角上的边界层,并且明显改变了流向速度的分布。然后,喷射羽流前方的分离区域更靠近壁,并且喷射羽流上风侧的大型涡旋的破裂过程更早开始。然而,由壁膨胀产生的有利的压力梯度降低了混合效率并且带来了更大的总压力损失。

著录项

  • 来源
    《Acta astronautica》 |2016年第12期|161-173|共13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;

    Natl Univ Def Technol, Sci & Technol Scramjet Lab, Changsha 410073, Hunan, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    LES; Transverse jet; Expansion effect; Turbulent boundary layer; Favorable pressure gradients;

    机译:LES;横向射流;膨胀效应;湍流边界层;有利的压力梯度;

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