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Mixing enhancement of jets and drag reduction in manipulated bluff body wakes.

机译:喷射的混合增强和操纵虚张声势的身体尾流的阻力减小。

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摘要

In the first part of this work a direct numerical simulation of the approach is employed in the study of a planar jet immersed in a co-flowing stream. An aerodynamic vectoring effect on the jet is achieved by the application of asymmetrically distributed suction at the lips of the exit nozzle. An optimal suction distribution for maximum lift generation is located and used in conjunction with time-dependent stimulation to enhance the mixing characteristics of the jet. The dynamic behavior of the system in the phase plane is explored and a regime of suction parameters for maximum mixing enhancement is revealed. The attractor selection sensitivity to initial conditions of the system is also investigated.; The second part of this dissertation used direct numerical simulation in the study of the flow dynamics in the near wake of a two dimensional rectangular bluff body. The suppression of the global mode of instability via base suction or bleed is investigated and the ventilation coefficient cvent , a non-dimensional measure of the ventilation mass flux, is identified as a major scaling parameter in the determination of the structural characteristics and suppression of the global mode of via base bleed.; Aerodynamic drag reduction is pursued by modifying the base pressure component of the drag. Boat-tails (blocks and plates) are attached at the trailing edge of the rectangular forebody and an optimal aspect ratio for boat-tail notches at the separation point is identified. The use of boat-tailing in conjunction with base bleed is also investigated and the common underlying mechanism leading to elevated base pressure in different configurations is revealed.
机译:在这项工作的第一部分中,该方法的直接数值模拟被用于研究浸没在同流流中的平面射流。通过在出口喷嘴的唇缘处施加不对称分布的吸力,可以实现对射流的空气动力引导效果。找到最佳的吸力分布,以产生最大的升力,并与时间相关的刺激结合使用,以增强射流的混合特性。探索了系统在相平面中的动态行为,并揭示了用于最大程度增强混合效果的吸力参数方案。还研究了吸引子选择对系统初始条件的敏感性。本文的第二部分使用直接数值模拟研究了二维矩形钝体的近尾流动力学。研究了通过基础吸力或放气抑制整体不稳定性的方法,并且通气系数cvent是通气质量通量的无量纲度量,被确定为确定结构特性和抑制通气量的主要缩放参数。 via基地出血的全局模式。通过改变阻力的基本压力分量来追求减少气动阻力。船尾(块和板)固定在矩形前体的后缘,并确定了分离点处船尾缺口的最佳长宽比。还研究了船尾结合基础放气的使用,并揭示了导致不同构造中基础压力升高的常见潜在机理。

著录项

  • 作者

    Arcas, Diego Rodriguez.;

  • 作者单位

    University of Southern California.;

  • 授予单位 University of Southern California.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2003
  • 页码 163 p.
  • 总页数 163
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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