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    Aerodynamic Performance Evaluation of Subsonic Compressor Cascade Blade With Leading-Edge Damage 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 007:;page 71003-1
    Author(s): Zhang, Haideng; Wu, Yun; Long, Yuhan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Material loss at the leading edge of in-service gas-turbine engine blades is detrimental to the aerodynamic performances of compressors. In this study, computational simulations and experiments using pneumatic probes were ...
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    Runup of Laboratory-Generated Breaking Solitary and Periodic Waves on a Uniform Slope 

    Source: Journal of Waterway, Port, Coastal, and Ocean Engineering:;2018:;Volume ( 144 ):;issue: 006
    Author(s): Wu Yun-Ta;Liu Philip Li-Fan;Hwang Kao-Shu;Hwung Hwung-Hweng
    Publisher: American Society of Civil Engineers
    Abstract: In this article, we demonstrate that the normalized runup heights, R/H (R = runup height; H = incident wave height), for breaking solitary and periodic waves can be characterized by a single dimensionless parameter, called ...
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