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    On the Interactions of a Rotor Blade Tip Flow With Axial Casing Grooves in an Axial Compressor Near the Best Efficiency Point 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 001:;page 11008
    Author(s): Chen, Huang; Li, Yuanchao; Katz, Joseph
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments in a refractive index-matched axial turbomachine facility show that semicircular skewed axial casing grooves (ACGs) reduce the stall flowrate by 40% but cause a 2.4% decrease in the maximum efficiency. Aiming ...
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    Effects of Axial Casing Grooves on the Structure of Turbulence in the Tip Region of an Axial Turbomachine Rotor 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 009:;page 091009-1
    Author(s): Chen, Huang; Li, Yuanchao; Koley, Subhra Shankha; Katz, Joseph
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Challenges in turbulence modeling in the tip region of turbomachines include anisotropy, inhomogeneity, and non-equilibrium conditions, resulting in poor correlations between Reynolds stresses and the corresponding mean ...
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    Effect of Axial Casing Groove Geometry on Rotor-Groove Interactions in the Tip Region of a Compressor 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 009:;page 091010-1
    Author(s): Koley, Subhra Shankha; Chen, Huang; Saraswat, Ayush; Katz, Joseph
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This experimental study characterizes the interactions of axial casing grooves (ACGs) with the flow in the tip region of an axial turbomachine. The tests involve grooves with the same inlet overlapping with the rotor blade ...
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    Visualizations of Flow Structures in the Rotor Passage of an Axial Compressor at the Onset of Stall 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 004:;page 41008
    Author(s): Chen, Huang; Li, Yuanchao; Tan, David; Katz, Joseph
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments preformed in the JHU refractive index matched facility examine flow phenomena developing in the rotor passage of an axial compressor at the onset of stall. High-speed imaging of cavitation performed at low ...
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    Experimental Investigations of Cavitation Performance Breakdown in an Axial Waterjet Pump 

    Source: Journal of Fluids Engineering:;2020:;volume( 142 ):;issue: 009:;page 091204-1
    Author(s): Chen, Huang; Doeller, Nick; Li, Yuanchao; Katz, Joseph
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This experimental study examines the mechanisms causing cavitation breakdown in an axial waterjet pump. The database includes performance curves, images of cavitation, measured changes to endwall pressure as the blade ...
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    Effect of the Axial Casing Groove Geometry on the Production and Distribution of Reynolds Stresses in the Tip Region of an Axial Compressor Rotor 

    Source: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 009:;page 91007-1
    Author(s): Koley, Subhra Shankha; Saraswat, Ayush; Chen, Huang; Katz, Joseph
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Stereo-PIV data are used for investigating the effect of axial casing groove (ACG) geometry on the distribution, evolution, and production rates of turbulent kinetic energy (TKE) and Reynolds stresses near a rotor tip. The ...
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    Volatilization Characteristics of Organic Compounds in the Coagulation Process 

    Source: Journal of Environmental Engineering:;2005:;Volume ( 131 ):;issue: 009
    Author(s): Huan-Ping Chao; Jiunn-Fwu Lee; Chung-Kung Lee; Hui-Chen Huang
    Publisher: American Society of Civil Engineers
    Abstract: The emissions of two types of organic solutes during the coagulation process were simulated using Jar Test equipment and two additives, coagulant and polymer, to evaluate the volatilization characteristics under various ...
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    Output-Constrained Attitude Tracking Control for Spacecraft with Adaptive Inertia and Disturbance Identifications 

    Source: Journal of Aerospace Engineering:;2023:;Volume ( 036 ):;issue: 005:;page 04023033-1
    Author(s): Qijia Yao; Qing Li; Chen Huang; Hadi Jahanshahi
    Publisher: ASCE
    Abstract: In this paper, we present an adaptive control strategy for the output-constrained attitude tracking of rigid spacecraft under unknown inertia and disturbances. The designed controller is recursively constructed under the ...
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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