Numerical and experimental study on air thrust foil bearing performance with improved structural model based on real-time taper inlet height Fangcheng Xu ( [email protected] ) Dalian University of Technology Liukai Hou Beijing Aerospace Propulsion Institute Bin Wu Suzhou Dongling Vibration Test Instrument Co., Ltd Zeda Dong Dalian University of Technology Yongliang Wang Dalian Maritime University Original Article Keywords: Air thrust foil bearing, Taper inlet height, Load capacity, Friction torque, Test Posted Date: July 8th, 2020 DOI: https://doi.org/10.21203/rs.3.rs-40416/v1 License: This work is licensed under a Creative Commons Attribution 4.0 International License. Read Full License
Numerical and experimental study on air thrust foil bearing performance with improved structural model based on real-time taper inlet height
Jul 01, 2023
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