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    Investigations on the Aerodynamic Performance of a Gas Turbine Exhaust Diffuser With the Modified Shell Profile 

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 144 ):;issue: 012:;page 121021
    Author(s): Dong, Yuxuan;Li, Zhigang;Li, Jun
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, a shell profile design method based on diffuser flow area curve is proposed to improve the static pressure recovery coefficient of the exhaust diffuser over a range of inlet swirl angles. Based on verifying ...
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    Investigations on the Splitter Structure to Improve the Aerodynamic Performance of Gas Turbine Exhaust Diffuser at Different Swirl Angles 

    Source: Journal of Engineering for Gas Turbines and Power:;2023:;volume( 145 ):;issue: 006:;page 61015-1
    Author(s): Dong, Yuxuan; Li, Zhigang; Li, Jun
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: To weaken the flow separation in the exhaust diffuser under real operating conditions and increase the static pressure recovery coefficient of the exhaust diffuser, an exhaust diffuser structure with splitters was proposed. ...
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    An Investigation of the Tapered Strut on Aerodynamic Performance of the Exhaust Diffuser Under Different Swirls 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 144 ):;issue: 001:;page 11006-1
    Author(s): Dong, Yuxuan; Li, Zhigang; Li, Jun
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The strut structure directly affects the flow-field characteristics and aerodynamic performance of the gas turbine exhaust diffuser. Based on verifying the reliability of the numerical method, the exhaust diffuser with ...
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