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Impact of Falling Blocks of High Pressure Turbine Rotor Blades With Squealer Tip on the Aerodynamic Performance and Vibration Characteristics
Power Generation Technology Vol. 45, Issue 5, Pages: 856-867(2024)
Gas Turbine Power Generation Technology|Updated：2025-06-15
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Impact of Falling Blocks of High Pressure Turbine Rotor Blades With Squealer Tip on the Aerodynamic Performance and Vibration Characteristics
- “In the field of gas turbines, experts have analyzed the impact of blade tip groove wear on aerodynamic performance and vibration deformation of high-pressure turbine blades through three-dimensional numerical simulation methods, providing a basis for evaluating the service status of turbine blades.”
DOI：10.12096/j.2096-4528.pgt.24094
Revised：2024-07-11
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Related Author
LI Shihan
BAI Bo
CHENG Guoqiang
XU Chengtian
KONG Xianglin
LI Zhigang
LI Jun
LU Wenqiang
Related Institution
State Key Laboratory of Clean and Efficient Turbomachinery Power Equipment
Dongfang Electric Corporation Dongfang Turbine Co., Ltd.
Institute of Turbomachinery, Xi’an Jiaotong University
University of Chinese Academy of Sciences, Haidian District
Nanjing Institute of Future Energy System, IET, CAS
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