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    Interaction Mechanism of Transonic Squealer Tip Cooling With the Effect of High-Speed Relative Casing Motion 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 008:;page 81016-1
    Author(s): Xie, W.; Lu, S.; Jiang, H.; Peng, X.; Zhang, Q.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The relative casing motion can significantly influence the turbine blade tip aerothermal performance. In this study, experimental investigation was conducted in a newly developed high-speed disk rotor rig which can mimic ...
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    A High-Speed Disk Rotor Rig Design for Tip Aerothermal Research 

    Source: Journal of Turbomachinery:;2021:;volume( 144 ):;issue: 005:;page 51002-1
    Author(s): Lu, S.; Zhang, Q.; He, L.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The relative casing motion can greatly vary the over-tip-leakage (OTL) flow structure and aerothermal performance. The existing tip experimental research facilities including stationary linear cascade, cascade rigs with ...
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    Experimental Evidence of Temperature Ratio Effect on Turbine Blade Tip Heat Transfer 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 012:;page 121010
    Author(s): Jiang, H.; Zhang, Q.; He, L.; Lu, S.; Wang, L.; Teng, J.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Determination of a scalable Nusselt number (based on “adiabatic heat transfer coefficient”) has been the primary objective of the most existing heat transfer experimental studies. Based on the assumption that the wall ...
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