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An investigation into the mechanisms of drag reduction of a boat tailed base cavity on a blunt based body.

机译:对钝基体上船尾基腔减阻机理的研究。

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摘要

It is well documented in the literature that boat-tailed base cavities reduce the drag on blunt based bodies. The majority of the previous work has been focused on the final result, namely reporting the resulting drag reduction or base pressure increase without examining the methods in which such a device changes the fluid flow to enact such end results. The current work investigates the underlying physical means in which these devices change the flow around the body so as to reduce the overall drag.;A canonical model with square cross section was developed for the purpose of studying the flow field around a blunt based body. The boat-tailed base cavity tested consisted of 4 panels of length equal to half the width of the body extending from the edges of the base at an angle towards the models center axis of 12°. Drag and surface pressure measurements were made at Reynolds numbers based on width from 2.3x105 to 3.6x10 5 in the Clarkson University high-speed wind tunnel over a range of pitch and yaw angles. Cross-stream hotwire wake surveys were used to identify wake width and turbulence intensities aft of the body at Reynolds numbers of 2.3x105 to 3.0x105. Particle Image Velocimetry (PIV) was used to quantify the flow field in the wake of the body, including the mean flow, vorticity, and turbulence measurements.;The results indicated that the boat-tailed aft cavity decreases the drag significantly due to increased pressure on the base. Hotwire measurements indicated a reduction in wake width as well as a reduction in turbulence in the wake. PIV measurements indicated a significant reduction in wake turbulence and revealed that there exists a co-flowing stream that exits the cavity parallel to the free stream, reducing the shear in the flow at the flow separation point. The reduction in shear at the separation point indicated the method by which the turbulence was reduced. The reduction in turbulence combined with the reduction in wake size provided the mechanism of drag reduction by limiting the rate of entrainment of fluid in the recirculating wake to the free stream and by limiting the area over which this entrainment occurs.
机译:在文献中有充分的文献证明,船尾基腔可减少对钝基体的阻力。先前的大部分工作都集中在最终结果上,即报告所产生的阻力减小或基础压力增加,而没有检查这种设备改变流体流量以实现这种最终结果的方法。当前的工作是研究这些设备改变身体周围流动以减少整体阻力的潜在物理手段。为了研究钝性物体周围的流场,开发了具有正方形横截面的规范模型。测试的船尾底腔由4个面板组成,这些面板的长度等于主体宽度的一半,从面板的边缘向模型中心轴倾斜12°延伸。在克拉克森大学高速风洞中,在一定的俯仰角和偏航角范围内,以基于2.3x105至3.6x10 5的宽度的雷诺数进行阻力和表面压力测量。跨流热线尾迹调查用于确定雷诺数为2.3x105至3.0x105时身体后部的尾迹宽度和湍流强度。粒子图像测速(PIV)用于量化人体苏醒后的流场,包括平均流量,涡度和湍流测量结果;结果表明,由于压力增加,船尾尾腔显着降低了阻力在基地上。热线测量表明,尾流宽度减小,尾流湍流减小。 PIV测量表明,尾流湍流显着减少,并且表明存在平行流与自由流平行离开腔体的同流流,从而减小了流分离点处的流切变。分离点处剪切力的降低表明了减少湍流的方法。湍流的减少与尾流尺寸的减小相结合,通过限制再循环尾流中流体向自由流的夹带速率并限制了夹带的发生面积,提供了减小阻力的机制。

著录项

  • 作者

    Kehs, Joshua Paul.;

  • 作者单位

    Clarkson University.;

  • 授予单位 Clarkson University.;
  • 学科 Engineering Aerospace.;Engineering Automotive.;Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2014
  • 页码 179 p.
  • 总页数 179
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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