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    Effects of Tip Gap Size on the Aerodynamic Performance of a Cavity-Winglet Tip in a Turbine Cascade 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 010:;page 101009
    Author(s): Zhong, Fangpan; Zhou, Chao
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aerodynamic performance of a cavity-winglet tip is investigated in a high-pressure turbine cascade by experimental and numerical methods. The winglet tip has geometric features of a cavity and a suction side fore-part ...
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    A Novel Suction-Side Winglet Design Philosophy for High-Pressure Turbine Rotor Tips 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 011:;page 111002
    Author(s): Zhou, Chao; Zhong, Fangpan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Winglet tips are promising candidates for future high-pressure turbine rotors. Many studies found that the design of the suction-side winglet is the key to the aerodynamic performance of a winglet tip, but there is no ...
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    Heat Transfer of Winglet Tips in a Transonic Turbine Cascade 

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 001:;page 12605
    Author(s): Zhong, Fangpan; Zhou, Chao; Ma, H.; Zhang, Q.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Understanding the heat transfer of winglet tips is crucial for their applications in high-pressure turbines. The current paper investigates the heat transfer performance of three different winglet-cavity tips in a transonic ...
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