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High-speed high-resolution vector field measurements and analysis of boundary layer flows in an internal combustion engine.

机译:内燃机的高速高分辨率矢量场测量和边界层流分析。

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摘要

Heat transfer properties vary locally and temporally in internal combustion engines due to variations in the boundary layer flow. In order to characterize the dynamics in the boundary layer, crank-angle resolved high-speed Micro Particle Image Velocimetry (muPIV) and Particle Tracking Velocimetry (PTV) have been used for near-wall velocity measurements in a spark-ignition direct-injection single cylinder engine. A 527 nm dual cavity green Nd:YLF laser was used for velocity measurements near the cylinder head wall between the intake and exhaust valves in the tumble mean flow plane parallel to the cylinder axis. A long distance microscope was used to obtain a spatial resolution of 45 mum. Flow fields were determined from 180 to 490 CAD in the compression and expansion strokes. The accomplished experiment represents first-time two-dimensional and a time history velocity measurements in a boundary layer flow in internal combustion engine. The data shows significant variation in the flow during the compression and expansion strokes and from cycle to cycle. Flow deceleration was observed during the end of the compression which continued during the expansion stroke until 400 CAD when the flow direction reverses. Submillimeter sized vortical structures were observed within the boundary layer over extended periods of time. Inner length and velocity scales were determined from the experimental results and were used to construct the law of the wall velocity distribution in the viscous sublayer and in the log law region. Experimental velocity profiles show agreement with the law of the wall in the viscous sublayer but they exhibit an early departure in the log law region due to the unique nature of the tumbling free stream flow in internal combustion engines. Reynolds stresses in the plane flow along with turbulent kinetic energy production and dissipation were determined.
机译:由于边界层流的变化,热传递特性在内燃机中局部地和临时地变化。为了表征边界层中的动力学特性,已将曲轴角分辨高速微颗粒图像测速仪(muPIV)和颗粒跟踪测速仪(PTV)用于火花点火直接喷射式单壁发动机的近壁速度测量。气缸发动机。使用527 nm双腔绿色Nd:YLF激光在平行于气缸轴线的滚流平均流平面中进气门和排气门之间的气缸盖壁附近进行速度测量。使用长距离显微镜获得45微米的空间分辨率。在压缩和膨胀冲程中确定的流场为180至490 CAD。完成的实验代表了内燃机边界层流中的首次二维和时程速度测量。数据显示在压缩冲程和膨胀冲程期间以及每个周期之间的流量有很大变化。在压缩结束时观察到流量减速,在膨胀冲程期间持续减速,直到流动方向反向时达到400 CAD。在延长的时间内,在边界层内观察到了亚毫米大小的涡旋结构。根据实验结果确定内部长度和速度尺度,并将其用于构造粘性子层和对数律区域中壁速度分布的规律。实验速度分布显示出与粘性子层中壁的定律一致,但是由于内燃机中自由流动的滚流的独特性质,它们在对数定律区域表现出较早的偏离。确定了平面流中的雷诺应力以及湍动能的产生和耗散。

著录项

  • 作者

    Alharbi, Ali.;

  • 作者单位

    University of Michigan.;

  • 授予单位 University of Michigan.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2010
  • 页码 140 p.
  • 总页数 140
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:37:09

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