首页> 外文学位 >Effect of finite cavity width on the self-sustained oscillation in a low-mach-number cavity flow.
【24h】

Effect of finite cavity width on the self-sustained oscillation in a low-mach-number cavity flow.

机译:有限腔体宽度对低马赫数腔体流动中自持振荡的影响。

获取原文
获取原文并翻译 | 示例

摘要

Cavity flow is known to be associated with high-level-noise generation, strong vibration and substantial increase in the drag force on the object containing the cavity. Most of the studies of the cavity flow are based on a two-dimensionality assumption. The three-dimensional features of cavity unsteadiness/oscillation are rarely investigated. The current study is focused on examining the effect of the cavity width and side walls on the self-sustained oscillation in a low-Mach-number cavity flow with a turbulent boundary layer at separation.;An axisymmetric cavity geometry is employed in the present research. The axisymmetric configuration provides a distinct advantage in studying the side-wall effects in that the configuration provides a reference condition that is free from any side-wall influence; yet, the cavity could be partially filled to form a finite-width geometry. Unsteady surface pressure, on the cavity floor along the streamwise direction and on the downstream wall along the azimuthal direction, is acquired using microphone arrays. The pressure data are recorded over a range of flow and geometrical parameters. In particular, the Reynolds number based on cavity depth and free-stream velocity is changed from Re = 4067 to 12200, and cavity length-to-depth ratio L/D from 2.6 to 4.1 for both the axisymmetric geometry and finite-width cavities with width-to-depth ratio W/D in the range 2.5 to 7.4. Based on the outcome of the analysis of the unsteady surface-pressure field, velocity measurements using a two-component Laser Doppler Anemometer (LDA) system are performed simultaneously with array measurements in different azimuthal planes for a cavity with L/D = 3.3 and W/D = 7.4 at Re = 12200 to explore the effect of the side wall on the mechanism driving the cavity oscillation. Evolution of coherent structures generating the pressure oscillation on the downstream wall of the cavity is evaluated using linear stochastic estimation (LSE) of the velocity field based on the wall-pressure signature.;The results show that while no prominent oscillation is found in axisymmetric cavities without side walls, strong harmonic pressure oscillation different from any of the known modes in the literature is observed in finite-width cavities at an azimuthal location of about one cavity depth away from the side wall. Analysis of the mean three-dimensional flow inside the cavity and the stochastic estimation results lead to the hypothesis that the flow structures in the symmetry plane of the finite-width cavities, although have a weak pressure signature, they interact with the flow near the side wall, providing the driving mechanism for the establishment of the oscillation near the side wall. Follow up experiments to validate this hypothesis are described.
机译:已知空腔流动与高水平的噪声产生,强烈的振动以及对包含空腔的物体的阻力的显着增加有关。大多数关于腔流的研究都是基于二维假设。很少研究空腔不稳定/振动的三维特征。目前的研究重点是在低马赫数的腔流中分离时带有湍流边界层的情况下,研究腔宽度和侧壁对自持振荡的影响。;本研究采用轴对称腔几何。轴对称构型在研究侧壁效应方面具有明显优势,因为该构型提供了不受任何侧壁影响的参考条件。但是,可以部分填充空腔以形成有限宽度的几何形状。使用传声器阵列获取沿流向的空腔底部和沿方位角的下游壁上的不稳定表面压力。在一定范围的流量和几何参数上记录压力数据。尤其是,对于轴对称几何形状和有限宽度的空腔,基于空腔深度和自由流速度的雷诺数从Re = 4067更改为12200,并且空腔长深比L / D从2.6变为4.1。宽深比W / D在2.5到7.4之间。根据非稳态表面压力场​​的分析结果,使用二分量激光多普勒风速计(LDA)系统进行速度测量,同时对L / D = 3.3和W的腔在不同方位平面中进行阵列测量/ D = 7.4,Re = 12200,以研究侧壁对驱动空腔振荡的机制的影响。基于壁压力特征,利用速度场的线性随机估计(LSE)评估了在腔体下游壁上产生压力振荡的相干结构的演化;结果表明,在轴对称腔体中未发现明显的振荡在没有侧壁的情况下,在距侧壁大约一个腔深度的方位角位置的有限宽度腔中观察到了与文献中任何已知模式不同的强谐波压力振荡。对腔体内平均三维流动的分析和随机估计结果得出这样的假设:有限宽度腔对称平面内的流动结构虽然具有较弱的压力特征,但它们与侧面附近的流动相互作用壁,为在侧壁附近建立振荡提供了驱动机制。描述了验证该假设的后续实验。

著录项

  • 作者

    Zhang, Ke.;

  • 作者单位

    Michigan State University.;

  • 授予单位 Michigan State University.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2009
  • 页码 150 p.
  • 总页数 150
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号