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Numerical Study of the Effects of Thermal Barrier Coating and Turbulence Intensity on Cooling Performances of a Nozzle Guide Vane

机译：热障涂层和湍流强度对喷嘴导叶冷却性能影响的数值研究

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Prasert Prapamonthon; Huazhao Xu; Wenshuo Yang; Jianhua Wang;
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1. Numerical Study of the Effects of Thermal Barrier Coating and Turbulence Intensity on Cooling Performances of a Nozzle Guide Vane [J] . Prasert Prapamonthon, Huazhao Xu, Wenshuo Yang, Energies . 2017,第3期

机译：热障涂层和湍流强度对喷嘴导流叶片冷却性能影响的数值研究
2. Experimental study of free-stream turbulence intensity effect on overall cooling performances and solid thermal deformations of vane laminated end-walls with various internal pin-fin configurations [J] . Applied thermal engineering: Design, processes, equipment, economics . 2020,第期

机译：自由流湍流强度效应对各种内部销翅片配置的叶片层压末端壁的整体冷却性能和固体热变形的实验研究
3. The Combined Influences of Film Cooling and Thermal Barrier Coatings on the Cooling Performances of a Film and Internal Cooled Vane [J] . Li Shi, Zhiying Sun, Yuanfeng Lu Coatings . 2020,第9期

机译：薄膜冷却和热阻挡涂层对薄膜和内冷叶片冷却性能的组合影响
4. NUMERICAL PREDICTION OF COOLING PERFORMANCE SENSITIVITY OF 1st STAGE NOZZLE GUIDE VANE UNDER AEROTHERMAL CONDITIONS [C] . Prasert Prapamonthon, Bo Yin, Guowei Yang, ASME gas turbine India conference . 2019

机译：一级温度条件下第一级导流叶片冷却性能敏感性的数值预测
5. Degradation of thermal barrier coatings on an Integrated Gasification Combined Cycle (IGCC) simulated film-cooled turbine vane pressure surface due to particulate fly ash deposition [D] . Luo, Kevin 2014

机译：由于颗粒飞灰的沉积，整体气化联合循环（IGCC）模拟的薄膜冷却涡轮叶片压力表面上的隔热涂层性能下降
6. Effect of Turbulence Intensity on Cross-Injection Film Cooling at a Stepped or Smooth Endwall of a Gas Turbine Vane Passage [O] . Pey-Shey Wu, Shen-Ta Tsai, Yue-Hua Jhuo -1

机译：湍流强度对燃气轮机叶片通道的阶梯形或光滑端壁处的交叉喷射薄膜冷却的影响
7. The Combined Influences of Film Cooling and Thermal Barrier Coatings on the Cooling Performances of a Film and Internal Cooled Vane [O] . Li Shi, Zhiying Sun, Yuanfeng Lu 2020

机译：薄膜冷却和热阻挡涂层对薄膜和内冷叶片冷却性能的组合影响

Numerical Study of the Effects of Thermal Barrier Coating and Turbulence Intensity on Cooling Performances of a Nozzle Guide Vane

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