Heat transfer of a rotating two-inlet trailing edge channel with lateral fluid extractions
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Heat transfer of a rotating two-inlet trailing edge channel with lateral fluid extractions

机译:具有横向流体提取的旋转双入口后边缘通道的传热

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摘要

AbstractAn experimental investigation of heat transfer in a radially rotating wedge-shaped channel with two inlets and lateral fluid extractions was conducted. The lateral inlet, comprising eight circular holes uniformly distributed on the wide sidewall, is for a second coolant besides the usual bottom inflow. The mass flow rate ratio (MR, lateral-to-total) is varied from 0 to 1.0 in current study to indicate the strength of the two streams. The major Reynolds number ranges from 10,000 to 20,000, and the highest rotation number is 1.1 in present work. In the current fashion of experiments, the effects of rotation number and buoyancy number could not be decoupled since the temperature ratio is controlled at around 0.14 in all the cases. Therefore, the authors would like to caution the audiences that there are uncontrollable buoyancy magnitude in the studies of the effects of rotation number. Compared with pure bottom inlet, higher heat transfer coefficients and better uniformity are observed with single lateral inlet. With both inlets, the increase ofMRenhances the heat transfer rates over the top-half regions at the expense of weakening the bottom-half counterparts; while the least heat transfer difference is obtained whenMRreaches 0.55. The averaged regional/surface heat transfer variations induced by rotation are no more than 6% whenMRexceeds 0.5. It is recommended that more coolant should be supplied to the lateral inlet due to higher heat transfer levels with lower heat transfer variations. Meanwhile, comparison with our previous works is performed both at static states and rotation states and some meaningful results are obtained.]]>
机译:<![CDATA [ 抽象 对具有两个入口和横向流体提取的径向旋转楔形通道中的传热的实验研究。包括均匀分布在宽侧壁上的八个圆孔的横向入口,除了通常的底部流入之外,对于第二冷却剂。质量流量比( mr ,横向 - 总)在当前研究中的0到1.0变化,以指示两个流的强度。主要雷诺数的数量从10,000到20,000,最高的旋转数为1.1。在当前的实验中,由于温度比在所有情况下控制约0.14,因此无法解耦旋转数量和浮力数的影响。因此,作者想警告观众,在旋转数量的影响中存在无法控制的浮力程度。与纯底部入口相比,用单侧入口观察到更高的传热系数和更好的均匀性。通过两个入口,增加 mr 以削弱下半部分对应物的牺牲增强了上半区域的传热速率;虽然当 Mr 达到0.55时,获得最小传热差异。当 mr 超过0.5时,通过旋转引起的平均区域/表面传热变化不超过6%。建议由于具有较低传热变化的热传递水平,应将更多的冷却剂供应到横向入口。同时,与我们以前的作品的比较是在静态状态和旋转状态下进行的,并且获得了一些有意义的结果。 ]>

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  • 作者单位

    National Key Laboratory of Science and Technology on Aero-Engines School of Energy and Power Engineering Beijing University of Aeronautics and Astronautics;

    National Key Laboratory of Science and Technology on Aero-Engines School of Energy and Power Engineering Beijing University of Aeronautics and Astronautics;

    National Key Laboratory of Science and Technology on Aero-Engines School of Energy and Power Engineering Beijing University of Aeronautics and Astronautics;

    National Key Laboratory of Science and Technology on Aero-Engines School of Energy and Power Engineering Beijing University of Aeronautics and Astronautics;

    R&

    D Center Dept of Discipline Engineering;

    National Key Laboratory of Science and Technology on Aero-Engines School of Energy and Power Engineering Beijing University of Aeronautics and Astronautics;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 热力工程、热机;
  • 关键词

    Trailing edge channel; Rotating heat transfer; Two inlets; Mass flow ratio;

    机译:后缘通道;旋转传热;两个入口;质量流量;

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