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The application of similarity theory for heat transfer investigation in rotational internal cooling channel

机译:相似理论在旋转内部冷却通道传热研究中的应用

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摘要

Full-scale test for turbine blade internal cooling is difficult for laboratory researches. The original turbine blade channel is always proportionally scaled up to laboratory-scale channel, as well as its hydraulic diameter and rotating radius. But the proportion scale of radius is too large for any rotating rig to operate the test, and thus the insufficient rotating radius causes incomplete similarity application. Because of the dissimilar radius induced incomplete similarity, heat transfer results obtained in laboratory-scale channel cannot be directly used by actual turbine blade design process. Therefore, this paper deals with this problem and numerically studies the influence of incomplete similarity through a rotating square channel with smooth walls and radially outward flow. Dimensionless parameters analysis demonstrates that the radius ratio (R/D) only shows influence on the buoyancy number (Buo) which causes much smaller buoyancy number for dissimilar model. Thus, three models with various scales and rotating radius are built. Model 1 is the original channel simplified from actual turbine blade internal cooling channel; Model 2 (similar model) and Model 3 (experimental model) are the corresponding scaled-up channels from Model 1 with complete similar radius and insufficient radius respectively. And two correction methods (variable radius and variable wall temperature) are developed to revise the influence caused by incomplete similarity of Model 3. Variable radius is used to vary rotating radius and variable wall temperature is used to vary wall temperature. The simulation is completed using commercial CFD solver and k-ω turbulent model. Result shows that the conventional application of similarity theory can predict heat transfer well for complete similar model (Model 2), but with a large deviation for dissimilar model (Mode 3). Given the same Re and Ro, the smaller Buo in Model 3 causes over 17% deviation heat transfer result. Then, the two revised methods concerning the effect of rotational radius ratio and wall temperature ratio are detailedly discussed, and both of them show less than 3% deviation in heat transfer distribution results. The detailed revised steps are also provided for both methods.
机译:实验室研究很难对涡轮叶片内部冷却进行全面测试。原始涡轮叶片通道及其液压直径和旋转半径始终按比例放大到实验室规模的通道。但是半径比例比例对于任何旋转钻机都无法操作,因此旋转半径不足会导致相似性应用不完全。由于不同的半径引起不完全相似,因此在实验室规模的通道中获得的传热结果无法直接用于实际的涡轮叶片设计过程。因此,本文针对此问题进行了处理,并通过旋转的方管,光滑的壁和径向向外流动的数值研究了不完全相似的影响。无量纲参数分析表明,半径比(R / D)仅显示对浮力数(Buo)的影响,对于不同模型,该值导致浮力数小得多。因此,建立了具有不同比例和旋转半径的三个模型。模型1是从实际涡轮叶片内部冷却通道简化而来的原始通道;模型2(相似模型)和模型3(实验模型)是模型1中相应的按比例放大的通道,分别具有完全相似的半径和不足的半径。并且开发了两种校正方法(可变半径和可变壁温)来修正由于模型3不完全相似而造成的影响。可变半径用于改变旋转半径,可变壁温用于改变壁温。使用商用CFD求解器和k-ω湍流模型完成了仿真。结果表明,相似理论的常规应用可以很好地预测完全相似模型(模型2)的传热,而对于相似模型(模型3)则有较大的偏差。在相同的Re和Ro的情况下,模型3中较小的Buo会导致超过17%的偏差传热结果。然后,详细讨论了两种有关旋转半径比和壁温比的影响的修改方法,它们在传热分布结果中均显示出小于3%的偏差。还为这两种方法提供了详细的修订步骤。

著录项

  • 来源
  • 作者单位

    National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics & Collaborative Innovation Center of Advanced Aero-Engine, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;

    National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics & Collaborative Innovation Center of Advanced Aero-Engine, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;

    National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics & Collaborative Innovation Center of Advanced Aero-Engine, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;

    National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics & Collaborative Innovation Center of Advanced Aero-Engine, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;

    Shenyang Aero-Engine Design and Research Institute, Aviation Industry Corporation of China, Shenyang 110015, China;

  • 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

    Similarity theory; Heat transfer; Rotating channel; Dissimilar radius; Scaled-up channel;

    机译:相似理论;传播热量;旋转通道;半径不同;扩大渠道;

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