研究论文
Turbine nozzle endwall aero-thermal characteristics under combustor louver coolant with interface cavity
Kaiyuan Zhang, Zhiyu Li, Jun Wu, Zhigang Li, Jun Li
Xi'an Jiaotong University Wuhan Ship Development & Design Institute
来源Applied Thermal Engineering
年份2022
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学术脉络
学科主题
工程Turbomachinery Performance and Optimization
Heat Transfer Mechanisms · Heat transfer and supercritical fluids
参考文献 39
Advanced impingement/film-cooling schemes for high-temperature gas turbines : numerical study
被引 7A. Immarigeon · Spectrum Research Repository (Concordia University) · 2003
Effect of discrete-hole arrangement on film-cooling effectiveness for the endwall of a turbine blade cascade
被引 56Francesca Satta, Giovanni Tanda · Applied Thermal Engineering · 2015
Gas Turbine Heat Transfer and Cooling Technology
被引 1,462Je-Chin Han, Sandip Dutta, Srinath V. Ekkad · CRC Press eBooks · 2012
此处列出前 3 条
引用本文 9
Effects of proactive phantom cooling on turbine endwall aerodynamic and film cooling performances considering aggressive swirling inflow
被引 11Zhiyu Li, Kaiyuan Zhang, Zhigang Li · Applied Thermal Engineering · 2023
Parameter sensitivity analysis of the interaction between purge flow and mainstream
被引 8Hongyu Gao, Yifei Dong, Xueying Li · Applied Thermal Engineering · 2024
Uncertainty quantification of turbine endwall aero-thermal performance under combustor-turbine interface louver coolant and cavity
被引 7Kaiyuan Zhang, Zhiyu Li, Zhiyu Li · Applied Thermal Engineering · 2024
按被引量排序，此处列出前 3 条