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    Experimental and Numerical Investigation of High Load Turbine Blade Tip Cavity Structures 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 006:;page 61008-1
    Author(s): Chen, Yingjie; Jiang, Dengyu; Du, Zhengshuai; Wang, Songtao
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Leakage flow loss is an important factor affecting the aerodynamic efficiency of turbines. In this paper, experimental and numerical computational studies were used to investigate three different tips of a highly loaded ...
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    Near Tip Loss Control With a Winglet Baffle Cavity Tip in a Turbine Cascade 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 010:;page 0101007-1
    Author(s): Li, Li; Jiang, Dengyu; Zhou, Chao; Luo, Hualing; Hou, Weitao; Chang, Qiyue
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aerodynamic performance of a winglet baffle cavity tip is investigated at different inlet incidences from −12.5 to +12.5 deg. This blade tip shows a geometry feature with a pressure side winglet and a baffle within the ...
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