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Numerical modeling on pumping performance of piccolo-tube multi- nozzles supersonic ejector in an oil radiator passage

机译:微型油管多喷嘴超音速喷射器在机油散热器通道中泵送性能的数值模拟

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摘要

A special issue concerned in the current study is the supersonic ejector-based cooling system in an oil radiator air-cooled passage. To match the geometric feature of mixing chamber (variable sectional configuration with a big aspect ratio of cross section), a novel piccolo-tube multi-nozzles supersonic ejector is designed and numerically assessed. In the current 3-D numerical simulations, a simplified approach by utilizing an isotropic porous medium model is adopted for modeling the flow through a compact oil radiator. Simultaneously, a scaled-model experimental test is conducted for the purpose of validation. From a scaled-model test, it is suggested that the CFD simulation based on the porous medium approach is generally acceptable. In the presence of porous matrix, approximately 20%–40% decrease of the ejector pumping ratio is produced in relative to the situation without oil radiator, due to the flow resistance across the porous matrix. A conjunctive parameter considering the nozzle numbers, nozzle throat diameter, and piccolo-tube length is proposed. Either from the CFD-based analysis or from the scaled-model test, it is confirmed that there is an optimal conjunctive parameter for achieving the best ejector performance.
机译:当前研究中涉及的一个特殊问题是油散热器空气冷却通道中基于超音速喷射器的冷却系统。为了匹配混合室的几何特征(横截面的长径比大的可变截面构造),设计并数值评估了一种新型的短笛管式多喷嘴超音速喷射器。在当前的3D数值模拟中,采用了一种利用各向同性多孔介质模型的简化方法来模拟通过紧凑型油散热器的流动。同时,为了验证的目的,进行了比例模型实验测试。根据比例模型测试,建议基于多孔介质方法的CFD模拟通常是可以接受的。在存在多孔基质的情况下,由于在多孔基质上的流动阻力,与没有油散热器的情况相比,喷射器的泵送比降低了约20%–40%。提出了考虑喷嘴数量,喷嘴喉径和短管长度的组合参数。从基于CFD的分析或缩放模型测试中,都可以确认存在一个最佳的联合参数,可以实现最佳的喷射器性能。

著录项

  • 来源
    《Energy》 |2018年第1期|216-227|共12页
  • 作者单位

    College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics;

    College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics,Collaborative Innovation Center of Advanced Aero-Engine;

    College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics;

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

    Oil radiator air-cooled passage; Ejector; Piccolo-tube nozzle; Porous medium model; Scaled model test;

    机译:机油散热器风冷通道;喷射器;短管喷嘴;多孔介质模型;比例模型试验;

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