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Large-Eddy Simulation of Time Evolution and Instability of Highly Underexpanded Sonic Jets

机译:高度超扩声速射流的时间演化和不稳定性的大涡模拟

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摘要

High-pressure jet injection into quiescent air is a challenging fluid dynamics problem in the field of aerospace engineering. Although plenty of experimental, theoretical, and numerical studies have been conducted to explore this flow, there is a dearth of literature detailing the flow evolution and instability characteristics, which is vital to the mixing enhancement design and jet noise reduction. In this paper, a density-based solver for compressible supersonic flow, astroFoam, is developed based on the OpenFOAM library. Large-eddy simulations of highly underexpanded jets with nozzle pressure ratios from 5.60 to 11.21 at a Reynolds number around 10(5) are carried out with a highresolution grid. A grid-convergence study has been conducted to confirm the fidelity of the large-eddy simulation results. The large-eddy simulation results have also been validated against available literature data in terms of the time-averaged near-field properties of underexpanded jets. The turbulent transition processes are revealed based on the instantaneous flow features and are quantitatively resolved according to the jet penetration and maximum width. The vorticity analysis is conducted to understand the turbulent transition mechanism, and it is found that the vortex stretching term plays a leading role on the distortion of the vortex rings in the near field of the jets. The dominant instability modes of jets, visualized by helicity, are quantitatively revealed based on the spectrum and relative phase of pressure fluctuation. The single helical modes corresponding to a phase angle close to +/- 180 deg with the 1 + 1 helices are dominant for nozzle pressure ratios of 5.60 and 7.47, whereas the complex and multiple helices for the other two higher nozzle pressure ratios are due to the superposition of the single and double helical modes. In addition, the performance of the coarse mesh and different subgrid-scale models on capturing the dominant instability characteristics in large-eddy simulation of underexpanded jets is investigated.
机译:向静态空气中高压喷射是航空航天工程领域中一个充满挑战的流体动力学问题。尽管已经进行了大量的实验,理论和数值研究来探索这种流动,但是缺乏详细的文献来详细描述流动的演变和不稳定特性,这对于混合增强设计和降低射流噪声至关重要。在本文中,基于OpenFOAM库开发了基于密度的可压缩超声速求解器astroFoam。在高分辨率网格下,对雷诺数为10(5)的喷嘴压力比为5.60至11.21的高度过度膨胀的射流进行大涡模拟。进行了网格收敛研究以确认大涡模拟结果的保真度。大涡模拟结果也已根据现有文献数据进行了验证,包括膨胀不足射流的时间平均近场特性。基于瞬时流动特征揭示了湍流过渡过程,并根据射流穿透力和最大宽度对其进行了定量解析。进行了涡度分析以了解湍流过渡机理,并且发现涡旋拉伸项对射流近场中涡旋环的畸变起着主导作用。根据压力波动的频谱和相对相位,定量揭示了螺旋桨可视化的主要失稳模式。对应于1 + 1螺旋的相角接近+/- 180度的单螺旋模式在5.60和7.47的喷嘴压力比中占主导地位,而其他两个较高的喷嘴压力比的复螺旋和多重螺旋则是由于单螺旋和双螺旋模式的叠加。此外,还研究了粗网格和不同子网格比例模型在捕获未充分膨胀射流的大涡流模拟中主导失稳特征方面的性能。

著录项

  • 来源
    《AIAA Journal》 |2016年第10期|3191-3211|共21页
  • 作者

    Li Xiaopeng; Yao Wei; Fan Xuejun;

  • 作者单位

    Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China;

    Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China;

    Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, 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

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