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    Flow Control of Annular Compressor Cascade by Synthetic Jets 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 002:;page 21018
    Author(s): Xinqian Zheng; Sheng Zhou; Yajun Lu; Anping Hou; Qiushi Li
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation conducted in a stationary annular cascade wind tunnel demonstrated that unsteady flow control using synthetic jets (zero mass flux) could effectively reduce flow ...
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    Separation Control of Axial Compressor Cascade by Fluidic-Based Excitations 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 004:;page 41016
    Author(s): Xinqian Zheng; Weidong Xing; Junyue Zhang; Yangjun Zhang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Flow separation control was investigated on a compressor cascade using three types of fluidic-based excitations: steady suction, steady blowing, and synthetic jet. By solving unsteady Reynolds–averaged ...
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    Stability Improvement of a High-Pressure Ratio Centrifugal Compressor by Flow Injection 

    Source: Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 006
    Author(s): Wenchao Zhang; Xiao He; Baotong Wang; Zhenzhong Sun; Xinqian Zheng
    Publisher: ASCE
    Abstract: High-pressure ratio centrifugal compressors are required in modern turboshaft engines with the requirements of a high power-to-weight ratio and low fuel consumption. The reduction of the stable flow range is one of 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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