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    Study of Starting Problem of Axisymmetric Divergent Dual Throat Nozzle 

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 006:;page 62602
    Author(s): Wang, Yangsheng; Xu, Jinglei; Huang, Shuai
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Compared to the conventional axisymmetric dual throat nozzle, the axisymmetric divergent dual throat nozzle (ADDTN) can offer larger thrust vector angles. However, the starting problem maybe exists in the ADDTN and results ...
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    Design and Preliminary Analysis of the Variable Axisymmetric Divergent Bypass Dual Throat Nozzle 

    Source: Journal of Fluids Engineering:;2020:;volume( 142 ):;issue: 006
    Author(s): Wang, Yangsheng; Xu, Jinglei; Huang, Shuai; Jiang, Jingjing; Pan, Ruifeng
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbofan engines with afterburners usually have variable nozzle throat area, and the nozzle throat area may increase by 50–100% during afterburning. An axisymmetric divergent bypass dual throat nozzle (ADBDTN) can offer ...
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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian