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Model of the Trajectory of an Inclined Jet in Incompressible Crossflow

机译:不可压缩横流中斜射流的轨迹模型

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摘要

A simple model of the flowfield induced by an inclined jet into an incompressible crossflow is proposed. In general, such a jet generates an asymmetric pair of vortices, with a larger one farther from the wall. The model accounts for the influence of the jet pitch angle beta (with respect to the wall), skew angle (with respect to the freestream direction), and velocity ratio r (the jet velocity to the freestream velocity) on the jet trajectory in the transverse plane in the far field. From the model, the increase of the jet penetration and the circulation of the large vortex in the transverse plane to the downstream distance x obeys to the same one-third law in the case of normal transverse jet. Data from the literature are normalized and compared to the model. Although there is considerable scatter, the normalized data are generally in accord with the predictions of the model. However, for low velocity ratios <= 1.0 when skew angle is near 90 deg, the effect of jet entrainment, and the effect of the horseshoe and wake vortices, may create a low-pressure region on the wall and hence alter the jet trajectory and influence the circulation.
机译:提出了由倾斜射流引起的不可压缩横流的流场的简单模型。通常,这种射流会产生一对不对称的涡流,且涡流的对角距壁较远。该模型考虑了射流俯仰角β(相对于壁),偏斜角(相对于自由流方向)以及速度比r(射流速度与自由流速度)对射流轨迹的影响。远场的横向平面。根据该模型,在正常横向射流的情况下,射流穿透的增加以及横向平面中大涡流向下游距离x的服从相同的三分之一定律。将来自文献的数据归一化并与模型进行比较。尽管存在很大的分散性,但是归一化的数据通常与模型的预测一致。但是,当偏角接近90度时,对于低速比<= 1.0,射流夹带的作用以及马蹄和尾流涡流的作用可能会在壁上形成低压区域,从而改变射流的轨迹并影响流通。

著录项

  • 来源
    《AIAA Journal》 |2018年第2期|458-464|共7页
  • 作者单位

    Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China;

    Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China;

    Univ Washington, Dept Aeronaut & Astronaut, Seattle, WA 98195 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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