Numerical simulations of flow fields and heat transfer characteristics in Tenon joint gap between turbine blade and disk under rotating conditions

被引:0
作者
Chen, Da-Wei [1 ]
Zhu, Hui-Ren [1 ]
Xu, Yang [1 ]
Jia, Xiao-Meng [1 ]
Liu, Cong [1 ]
Lu, Hai-Ying [2 ]
机构
[1] Northwestern Polytechnical University, Xi'an,710072, China
[2] AVIC Shenyang Aircraft Engine Design Institute, Shenyang,110000, China
来源
Proceedings of the ASME Turbo Expo | 2017年 / 5B-2017卷
关键词
601.2 Machine Components - 612.3 Gas Turbines and Engines - 617 Turbines and Steam Turbines - 631.1 Fluid Flow; General - 641.2 Heat Transfer;
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