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    Pulsed Suction Control in a Highly Loaded Compressor Cascade With Low Suction Flowrates 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 006:;page 061006-1
    Author(s): Zhang, Hongxin; Chen, Shaowen
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The influence of pulsed suction (PS) on flow separation and aerodynamic performance in a highly loaded compressor cascade is experimentally studied herein. The excitation frequency is investigated as it determines the ...
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    Aerodynamic Performance and Leakage Flow in Turbine Cascades With Sweeping Jet Actuators 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 006:;page 61015-1
    Author(s): Chen, Shaowen; Li, Weihang; Yang, Pengcheng; Liu, Yueqi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In recent years, unsteady flow-control technology has been considered as more promising for reducing secondary flow loss in turbines. Sweeping jet actuators (SJAs), in particular, have steadily been used in turbomachinery ...
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    Corner Separation Control Using Sweeping Jet Actuator in a Compressor Cascade 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 010:;page 104503-1
    Author(s): Yang, Pengcheng; Chen, Shaowen; Liu, Guanyu; Xu, Chen
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the pursuit of advancing active flow control (AFC) technology, a more promising nonsteady actuator known as sweeping jet actuator (SJA) has been equipped on the endwall to manage the corner separation in a compressor ...
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    Effects of Double-Side Labyrinth Seals on Aerodynamic Performance in a Transonic Shrouded Turbine Stage 

    Source: Journal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 002
    Author(s): Li, Weihang; Chen, Shaowen; Liu, Hongyan; Zhou, Zhihua; Wang, Songtao
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Labyrinth seals on both rotor casing and blade tip as an effective method to control the leakage flowrate of the shroud and improve aerodynamic performances in a transonic turbine stage are investigated in this study. ...
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    Experimental Study on Controlling Flow Separation of Compressor Cascades With Self-Excited Sweeping Jet Actuator 

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 009:;page 91014-1
    Author(s): Zeng, Cong; Chen, Shaowen; Zheng, Longye; Zhang, Yimin; Wang, Shiqi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The sweeping jet actuator (SJA), widely studied as a potential flow control method in compressors and turbines, results in unnecessary performance losses due to its requirement for additional energy and mass input. In this ...
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    Experimental Investigation for Flow Regime Identification Using Probability Density Function of Void Fraction Signals 

    Source: Journal of Fluids Engineering:;2020:;volume( 142 ):;issue: 006
    Author(s): Lin, Min-Song; Chen, Shao-Wen; Kuo, Feng-Jiun; Cheng, Yen-Shih; Ruan, Pei-Syuan; Hsu, Yon-Min; Lee, Jin-Der; Pei, Bau-Shei
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this study, upward air–water two-phase flow tests were carried out in a 3 cm diameter pipe under atmospheric pressure, and over 3000 data points were collected from a wide range of superficial gas and liquid velocities ...
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    Investigation on Variations of Void Fraction in a Subcooled Boiling Channel Under Vertical Forced Excitations 

    Source: Journal of Fluids Engineering:;2021:;volume( 143 ):;issue: 006:;page 061405-1
    Author(s): Chen, Shao-Wen; Lee, Wei-Cheng; Chang, Yu-Hsien; Ho, Ailing; Lee, Jin-Der; Yang, Jung-Hua; Wang, Jong-Rong
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental tests were carried out to investigate the vertically forced excitation effects on the subcooled boiling flow. The heated circular channel with an inner diameter of 11.9 mm was operated with various heat fluxes ...
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