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首页> 外文期刊>Journal of Flow Visualization and Image Processing >PIV OBSERVATION OF PREWHIRL FLOW UPSTREAM OF A TURBOPUMP INDUCER
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PIV OBSERVATION OF PREWHIRL FLOW UPSTREAM OF A TURBOPUMP INDUCER

机译:涡轮增压器涡流上游的PIV观察

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摘要

Complex flow caused by prewhirl flow, backflow, tip leakage flow, and main flow was determined in the inlet of a turbopump inducer by means of PIV. The prewhirl flow component swirled in the same direction as the inducer rotation along a casing from the inducer inlet to a region further upstream. A strong Reynolds shear stress occurred upstream of the inducer. This area became unsteady due to shear flow caused by the interaction of the prewhirl flow and the main flow. The region which developed a strong mean vorticity was steady due to being not influenced either by both the Reynolds shear stress or by the fluctuation vorticity near the blade tip.
机译:由涡流,回流,叶尖泄漏流和主流引起的复杂流是通过PIV在涡轮泵诱导器的入口中确定的。预旋流分量沿与诱导器相同的方向从壳体的入口旋流到更上游的区域,沿着壳体旋转。雷诺强烈的切应力出现在诱导器的上游。由于预旋流和主流的相互作用引起的剪切流,该区域变得不稳定。由于不受雷诺剪切应力或叶尖附近波动涡度的影响,形成强平均涡度的区域是稳定的。

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  • 作者单位

    Engine System Group, Space Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA), JAPAN;

    rnEngine System Group, Space Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA), JAPAN;

    rnEngine System Group, Space Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA), JAPAN;

    rnEngine System Group, Space Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA), JAPAN;

    rnEngine System Group, Space Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA), JAPAN;

    rnAdvanced Propulsion Technology Research Group, Space Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA), JAPAN;

    rnFoundation for Promotion of Japan Aerospace Technology, JAPAN;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    PIV; inducer; backflow; prewhirl flow; vorticity; reynolds shear stress;

    机译:PIV;诱导剂回流;预旋流涡度雷诺剪切应力;

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