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    Transient Tip Clearance Prediction Model Considering Transient Radial Temperature Distribution of Discs in a Gas Turbine Engine 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 004:;page 41012-1
    Author(s): Wei, Jie; Yang, Heli; Zheng, Pengbo; Wang, Baotong; Zheng, Xinqian
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The tip clearance of turbomachinery components, such as compressor and turbine, significantly impacts the gas turbine engine performance, including the thrust and fuel consumption. Therefore, an appropriate prediction of ...
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    An Efficient Quantification Method Based on Feature Selection for High-Dimensional Uncertainties of Multistage Compressors 

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 145 ):;issue: 002:;page 21002-1
    Author(s): Wang, Junying; Zheng, Xinqian; Yang, Heli; Sun, Zhenzhong; Song, Zhaoyun; Fu, Yu
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Multistage compressors are widely used in aero-engines, gas turbines, and industrial compressors. However, many inevitable geometric/condition uncertainties will lead to low manufacturing qualified rate and severe performance ...
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