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Large-Eddy Simulations of a Cylindrical Film Cooling Hole

机译:圆柱薄膜冷却孔的大涡模拟

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摘要

Large-eddy simulations are used to explore the unsteady jet-in-crossflow interactions arising from discrete hole film cooling from a cylindrical hole. The numerical grids are created using GridPro and solved in OpenFOAM. A recycling-rescaling technique is used to generate a realistic turbulent incoming boundary layer upstream of injection. The simulations match the conditions of an experiment in the open literature for the robust validation of the numerical solution and turbulence modeling. The current study tests the ability of large-eddy simulations in predicting film cooling flows using detailed experimental measurements. The large-eddy simulation results compared favorably with the experimental data except in areas close to the injection site and close to the wall. Grid resolution is discussed in terms of the percent turbulent kinetic energy resolved and related to the success of the large eddy simulation predictions in different regions of the jet. No substantial benefit was seen by using a dynamic Smagorinsky model for the subgrid turbulent heat fluxes instead of a constant subgrid Prandtl number. The trajectories, spreading rates, and large turbulent structures of the jet are discussed in terms of the hydrodynamic parameters such as velocity ratio and momentum ratio.
机译:大涡流模拟用于探索由圆柱孔离散的孔膜冷却引起的不稳定的射流交叉流相互作用。数字网格是使用GridPro创建的,并在OpenFOAM中求解。循环再缩放技术用于在注入上游生成逼真的湍流进入边界层。模拟与开放文献中的实验条件相匹配,可以对数值解和湍流建模进行可靠的验证。当前的研究使用详细的实验测量值测试大涡流模拟预测薄膜冷却流量的能力。大涡模拟结果与实验数据相比好,除了靠近注射部位和靠近壁的区域。根据解决的湍流动能百分比讨论了网格分辨率,该分辨率与射流不同区域中大型涡流模拟预测的成功有关。通过使用动态Smagorinsky模型处理亚网格湍流热通量而不是使用恒定的亚网格Prandtl数,并没有看到任何实质性收益。根据流体动力学参数(如速度比和动量比)讨论了射流的轨迹,扩散速率和大的湍流结构。

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  • 来源
    《Journal of Thermophysics and Heat Transfer》 |2013年第2期|255-273|共19页
  • 作者单位

    University of Central Florida, Orlando, Florida 32816 Department of Mechanical, Materials and Aerospace Engineering, Laboratory for Turbine Aerodynamics, Heat Transfer, and Durability, Center for Advanced Turbine and Energy Research, Building 40, Room 307;

    University of Central Florida, Orlando, Florida 32816 Department of Mechanical, Materials and Aerospace Engineering, Laboratory for Turbine Aerodynamics, Heat Transfer, and Durability, Center for Advanced Turbine and Energy Research, Building 40, Room 407;

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

  • 入库时间 2022-08-18 03:01:22

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