Impact of Falling Blocks of High Pressure Turbine Rotor Blades With Squealer Tip on the Aerodynamic Performance and Vibration Characteristics
Gas Turbine Power Generation Technology|更新时间: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.”
Power Generation TechnologyVol. 45, Issue 5, Pages: 856-867(2024)
作者机构:
1.中国航发沈阳发动机研究所,辽宁省 沈阳市 110015
2.西安交通大学能源与动力工程学院,陕西省 西安市 710049
作者简介:
基金信息:
Key Project of the National Natural Science Foundation of China(51936008)
ZHAO Mingyang,YIN Linlin,WEI Wentao,et al.Impact of Falling Blocks of High Pressure Turbine Rotor Blades With Squealer Tip on the Aerodynamic Performance and Vibration Characteristics[J].Power Generation Technology,2024,45(05):856-867.
ZHAO Mingyang,YIN Linlin,WEI Wentao,et al.Impact of Falling Blocks of High Pressure Turbine Rotor Blades With Squealer Tip on the Aerodynamic Performance and Vibration Characteristics[J].Power Generation Technology,2024,45(05):856-867. DOI: 10.12096/j.2096-4528.pgt.24094.
Impact of Falling Blocks of High Pressure Turbine Rotor Blades With Squealer Tip on the Aerodynamic Performance and Vibration Characteristics