Detached Eddy Rotor/Stator Interaction Conjugate Simulations of Film-Cooled TXirbine Sections

机译：薄膜冷却TXirbine截面的分离式涡流转子/定子相互作用共轭模拟

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A conjugate detached-eddy rotor/stator interaction simulation of a single-stage, film-cooled high-pressure turbine mid-span section is presented. In regions where the local grid spacing is less than the turbulent mixing length, the detached-eddy turbulence model of Bush and Mani is used to predict the turbulent viscosity. Outside of those regions, the Wilcox two-equation k-ω turbulence model is used. Time-averaged and instantaneous results from the detached-eddy simulation (DES) are compared to results from a similar unsteady, film-cooled Reynolds-averaged Navier-Stokes (URANS) simulation, a detached-eddy uncooled, adiabatic wall simulation, as well as experimental data. The numerical techniques used in the procedure are described along with details of the turbine stage flow and thermal fields.

机译：提出了单级膜冷高压透平中跨段的共轭分离涡转子/定子相互作用仿真。在局部网格间距小于湍流混合长度的区域中，使用Bush和Mani的分离涡流湍流模型来预测湍流粘度。在这些区域之外，使用Wilcox二方程k-ω湍流模型。将分离涡模拟（DES）的时间平均和瞬时结果与类似的非稳态，薄膜冷却的雷诺平均Navier-Stokes（URANS）模拟，分离涡非冷却，绝热壁模拟的结果进行了比较作为实验数据。描述了该过程中使用的数值技术以及涡轮级流量和热场的详细信息。

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来源
《41st AIAA fluid dynamics conference and exhibit 2011》|2011年|p.885-896|共12页
会议地点 Honolulu HI(US)
作者
Joshua Gottlieb; Roger Davis; John P. Clark;
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作者单位

University of California, Davis, California, 95616;

University of California, Davis, California, 95616;

Air Force Research Laboratory, Wright-Patterson, Ohio. 45433;

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原文格式 PDF
正文语种 eng
中图分类流体动力学;
关键词
c_p: specific heat; k: thermal conductivity; M: Mach number; Pr: Prandtl number; T: Temperature; et al;

机译：c_p：比热； k：导热系数； M：马赫数； Pr：Prandtl号； T：温度；等;

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专利

1. Conjugate rotor-stator interaction procedure for film-cooled turbine sections [J] . Gottlieb Joshua, Davis Roger, Clark John Aircraft Engineering and Aerospace Technology . 2017,第3期

机译：薄膜冷却涡轮机部分的共轭转子-定子相互作用程序
2. Compressible Large Eddy Simulation of a Francis Turbine During Speed-No-Load: Rotor Stator Interaction and Inception of a Vortical Flow [J] . Trivedi Chirag Journal of Engineering for Gas Turbines and Power . 2018,第11期

机译：空转时弗朗西斯涡轮的可压缩大涡模拟：转子-定子相互作用和涡流的产生
3. Large eddy simulations and global stability analyses of an annular and cylindrical rotor/stator cavity limit cycles [J] . Queguineur Matthieu, Bridel-Bertomeu Thibault, Gicquel Laurent Y. M., Physics of fluids . 2019,第10期

机译：环形和圆柱形转子/定子腔间隔循环的大涡模拟和全局稳定性分析
4. Conjugate Rotor-Stator Interaction Procedure for Film-Cooled Turbine Sections [C] . Joshua Gottlieb, Roger Davis, John P. Clark AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition . 2011

机译：薄膜冷却涡轮截面的共轭转子-定子相互作用程序
5. Numerical simulation of a closed rotor-stator system using Large Eddy Simulation [D] . Amouyal, Solal Abraham Teva 2014

机译：大涡模拟的密闭转子-定子系统数值模拟
6. The prospect of using large eddy and detached eddy simulations in engineering design and the research required to get there [O] . Johan Larsson, Qiqi Wang -1

机译：在工程设计中使用大型涡流和分离涡流模拟的前景以及达到该目标所需的研究
7. Detached Eddy Simulation for the Stator-Rotor Interaction of the Compressor High-Pressure Cascade [O] . Fan FENG, Yao-bing XIAO 2017

机译：压缩机高压级联的定子转子相互作用的分离涡流模拟
8. Detached-Eddy Simulation of Flow Non-Linearity of Fluid-Structural Interactions Using High Order Schemes [R] . Zha, G., Wang, B. 2009

机译：采用高阶格式的流体 - 结构相互作用流动非线性的离散涡模拟

Detached Eddy Rotor/Stator Interaction Conjugate Simulations of Film-Cooled TXirbine Sections

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