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Experimental analysis of the effect of vibrational non-equilibrium on the decay of grid-generated turbulence.

机译:振动非平衡对格栅产生的湍流衰减影响的实验分析。

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摘要

The technical feasibility of hypersonic flight (i.e., re-entry, hypersonic flight vehicles, cruise missiles, etc.) hinges on our ability to understand, predict, and control the transport of turbulence in the presence of non-equilibrium effects. A theoretical analysis of the governing equations suggests a mechanism by which fluctuations in internal energy are coupled to the transport of turbulence. Numerical studies of these flows have been conducted, but limited computational power results in reduced fidelity. Experimental studies are exceedingly rare and, consequently, experimental data available to build and evaluate turbulence models is nearly non-existent.;The Decaying Mesh Turbulence (DMT) facility was designed and constructed to generate a fundamental decaying mesh turbulent flow field with passive grids. Vibrational non-equilibrium was achieved via a capacitively-coupled radio-frequency (RF) plasma discharge which required an operating pressure of 30 Torr. The flow velocity was 30 m/s. Data was recorded with each grid at multiple plasma powers (Off, 150 W, and 300 W). Over two terabytes of highly resolved (3,450 image pairs) two-dimensional particle image velocimetry (PIV) was acquired and archived. Temperature measurements were carried out using coherent anti-Stokes Raman spectroscopy (CARS).;The primary objective of this study was to answer the fundamental scientific question: "Does thermal non-equilibrium alter the decay rate of turbulence?" The results of this study show that the answer is "Yes." The results demonstrate a clear coupling between thermal non-equilibrium and turbulence transport. The trends observed agree with those expected based on an analysis of the Reynolds stress transport equations, which provides confidence in transport equation-based modeling. A non-trivial reduction (∼30%) in the decay rate downstream of the 300 W plasma discharge was observed. The data also show that the decay of TKE downstream of the plasma discharge was delayed (∼20% downstream shift). In addition, the thermal non-equilbrium was observed to have no effect on the transverse stress. This suggests that, for this flow, the energy dilatation terms are small and unaffected by the plasma discharge, which simplifies modeling.
机译:高超音速飞行的技术可行性(即再进入,高超音速飞行器,巡航导弹等)取决于我们在存在非平衡效应的情况下理解,预测和控制湍流传输的能力。对控制方程的理论分析提出了一种机制,通过该机制,内部能量的波动与湍流的传递耦合。已经对这些流进行了数值研究,但是有限的计算能力导致了降低的保真度。实验研究极为罕见,因此几乎没有可用于建立和评估湍流模型的实验数据。;设计并构建了衰减网格湍流(DMT)设施,以生成具有被动网格的基本衰减网格湍流场。振动非平衡是通过电容耦合射频(RF)等离子体放电实现的,该放电需要30 Torr的工作压力。流速为30m / s。使用多个等离子功率(关闭,150 W和300 W)在每个栅格上记录数据。采集并存档了超过2 TB的高度解析(3,450个图像对)的二维粒子图像测速仪(PIV)。使用相干反斯托克斯拉曼光谱(CARS)进行温度测量。这项研究的主要目的是回答一个基本的科学问题:“热非平衡会改变湍流的衰减率吗?”这项研究的结果表明答案是“是”。结果表明,热非平衡与湍流传输之间存在清晰的耦合。观察到的趋势与基于雷诺应力传输方程分析的预期趋势一致,这为基于传输方程的建模提供了信心。观察到300 W等离子放电下游衰减率的平凡下降(〜30%)。数据还显示,等离子放电下游的TKE衰减被延迟(下游漂移约20%)。另外,观察到热非耐高温对横向应力没有影响。这表明,对于这种流动,能量膨胀项很小,不受等离子体放电的影响,从而简化了建模。

著录项

  • 作者

    Fuller, T. J.;

  • 作者单位

    Texas A&M University.;

  • 授予单位 Texas A&M University.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2009
  • 页码 1022 p.
  • 总页数 1022
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:38:24

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