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Optical measurements of the effects on a boundary layer of puffing in a large scale buoyant plume.

机译:光学测量在浮力较大的羽流中对膨化边界层的影响。

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摘要

An experimental study has been performed on a buoyant helium plume with a 1 meter base diameter. A cone was immersed in the plume to determine the effect of plume puffing on the boundary layer along the cone. The plume with an immersed cone was also compared to an unobstructed plume. Two regions of two-dimensional velocity fields were measured using particle image velocimetry (PIV) simultaneously. Helium mass fraction was determined by seeding the helium with acetone vapor for planar laser-induced fluorescence (PLIF). Each test includes 7 to 11 puff cycles.; Several experimental and analytical techniques were developed. A cone was designed that could effectively transmit the UV laser sheet needed for whole field PIV measurements. A 12 cm by 8 cm boundary layer PIV region was situated within a 1 m by 1 m PIV whole field region, and both PIV regions were recorded simultaneously using the same light sheet, seed particles, and frame rate. Concentration field measurements were obtained simultaneously with the velocity field measurements using PLIF for a region 0.8 m high and 1 m wide. Whole field velocity fields were measured with centimeter resolution in two spatial dimensions with temporal resolution of 0.005 second for a multi-second test. Techniques were developed to produce PIV velocity vectors for a highly accelerating flow with large velocity gradients, to register each image to correct for distortion, and to align each image relative to another eliminating a major source of velocity vector error.; While Reynolds-averaged turbulent statistics indicate that the presence of the cone does not affect the overall plume behavior, mixing in a puffing plume with an immersed cone is suppressed relative to that in an unobstructed puffing plume. No separation of the boundary layer flow along the cone was observed given the spatial resolution of 0.3 cm. As the toroidal (puff) vortex propagates upward, measurements suggest that the boundary layer thins and freestream velocity increases at the vertical location of the vortex. The plume with an immersed cone revealed splitting toroidal vortices and smaller scale vortices near the cone surface. These vortices may contribute as much to boundary layer unsteadiness as the large-scale periodic toroidal vortices. The boundary layer within a buoyant plume is turbulent with the mean profile shape and thickness varying considerably over time. Additional tests of finer spatial resolution in the boundary layer PIV region that are synchronized with whole field measurements are needed to further quantify the boundary layer variance.
机译:已经对具有1米基本直径的浮力氦羽进行了实验研究。将锥体浸入羽流中,以确定羽流沿锥体边界层的膨化效果。还比较了具有浸没锥的羽状流和畅通无阻的羽状流。同时使用粒子图像测速仪(PIV)测量二维速度场的两个区域。氦的质量分数是通过用氦蒸气在氦气中注入用于平面激光诱导的荧光(PLIF)的方式确定的。每个测试包括7至11个抽吸周期。开发了几种实验和分析技术。设计了一个圆锥体,可以有效地透射全场PIV测量所需的UV激光片。一个12 cm x 8 cm边界层PIV区域位于1 m x 1 m的PIV全场区域内,并且使用相同的光片,种子粒子和帧速率同时记录了两个PIV区域。使用PLIF对0.8 m高和1 m宽的区域同时进行了浓度场测量和速度场测量。全场速度场以厘米分辨率在两个空间维度上进行测量,时间分辨率为0.005秒,以进行多秒测试。已开发出技术来产生具有大速度梯度的高度加速流的PIV速度矢量,以配准每个图像以校正畸变,并使每个图像相对于另一个对齐,从而消除了主要的速度矢量误差源。雷诺平均的湍流统计数据表明,圆锥体的存在不会影响整体羽流行为,但相对于畅通无阻的膨化羽流而言,在膨化羽流与浸没的圆锥体中的混合受到抑制。给定0.3 cm的空间分辨率,没有观察到沿锥边界流的分离。随着环形(粉扑)涡流向上传播,测量表明边界层变薄,自由流速度在涡流的垂直位置增加。带有浸没的圆锥体的羽流在圆锥体表面附近显示裂开的环形涡旋和较小尺度的涡旋。这些旋涡对边界层不稳定的影响可能与大规模周期性环形旋涡相同。浮羽内的边界层是湍流的,其平均轮廓形状和厚度随时间变化很大。需要与全场测量同步的边界层PIV区域中更精细的空间分辨率的其他测试,以进一步量化边界层方差。

著录项

  • 作者

    Gerhart, Andrew L.;

  • 作者单位

    The University of New Mexico.;

  • 授予单位 The University of New Mexico.;
  • 学科 Engineering Mechanical.; Physics Fluid and Plasma.; Physics Optics.
  • 学位 Ph.D.
  • 年度 2004
  • 页码 284 p.
  • 总页数 284
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;等离子体物理学;光学;
  • 关键词

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