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    Uncertainty Quantification on the Cooling Performance of a Transonic Turbine Vane With Upstream Endwall Misalignment 

    Source: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 012:;page 121004
    Author(s): Hao, Mingyang;Bai, Bo;Li, Yuanyuan;Li, Zhigang;Li, Jun
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: With increasing aerodynamic and thermal loads, film cooling has been a popular technology integrated into the design of the modern gas turbine vane endwall, especially for the first-stage vane endwall. A staggering amount ...
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    Uncertainty Analysis of Laser Drilling Imperfection and Impacts on the Cooling Performance of a Transonic Turbine Vane 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 004:;page 41016-1
    Author(s): Hao, Mingyang; Bai, Bo; Zhang, Jiawei; Li, Zhigang; Li, Jun
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: To ensure the durability and reliability of gas turbine, film cooling has been integrated into the design of the modern gas turbine vane endwall, especially for the first-stage vane endwall. Percussion laser drilling has ...
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    Experimental Study on the Endwall Aerothermal Performance of Turbine Cascades in a Novel Transient Test Facility 

    Source: Journal of Thermal Science and Engineering Applications:;2024:;volume( 016 ):;issue: 011:;page 111006-1
    Author(s): Bai, Bo; Hao, Mingyang; Li, Yuanyuan; Li, Zhigang; Li, Jun; Mao, Shuo; Ng, Wing F.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Linear turbine cascades have been widely used to conduct fundamental and applied investigations, but only a few transient test facilities with the linear turbine cascade are available in the open literature. A novel transient ...
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