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    A Pioneering Method for Reducing Water Droplet Erosion 

    Source: Journal of Fluids Engineering:;2018:;volume( 140 ):;issue: 006:;page 61401
    Author(s): Yao, Hong; Zhou, Xun
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Based on computational fluid dynamics and the finite volume method, water droplet erosion in the last stage of an industrial steam turbine was researched and the trajectories of the water droplets were traced by using the ...
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    Using a Bowed Blade to Improve the Supersonic Flow Performance in the Nozzle of a Supersonic Industrial Steam Turbine 

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 010:;page 102604
    Author(s): Yao, Hong; Zhou, Xun; Wang, Zhongqi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: For solar plants, waste-energy recovery, and turbogenerators, there is a considerable amount of waste energy due to low mass flow rate. Owing to the high specific power output and large pressure ratios across the turbine, ...
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    On the Aero-Thermal Performance of Rim Film Cooling in the Squealer Tip of a Linear Turbine Cascade 

    Source: ASME Journal of Heat and Mass Transfer:;2024:;volume( 146 ):;issue: 003:;page 33801-1
    Author(s): Luo, Lei; Zhao, Zhiqi; Qiu, Dandan; Wang, Songtao; Zhou, Xun; Wang, Zhongqi; Li, Guangchao
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present study proposes a novel rim film cooling design, motivated by the fact that the suction-side rim and the cavity floor near the leading edge of a conventional squealer tip with a camber-line film hole array are ...
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    Enhancing Aerodynamic Performance of a Non-Axisymmetric Endwall Contoured Cascade Through Section Profiling Method 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 012:;page 121004-1
    Author(s): Du, Zhengshuai; Cai, Le; Zeng, Jun; Chen, Yingjie; Zhou, Xun; Wang, Songtao
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Endwall contouring and 3D blade configurations are effective techniques for enhancing turbomachinery performance. The integration of these technologies is an important area of investigation. To continue the numerical and ...
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