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    Dynamic Experimental Investigations of a Bypass Dual Throat Nozzle

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 008::page 84501
    Author:
    Gu, Rui
    ,
    Xu, Jinglei
    DOI: 10.1115/1.4029391
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The bypass dual throat nozzle (BDTN) does not consume any secondary injection from the other part of the engine, while it can produce steady and efficient vectoring deflection similar to the conventional dual throat nozzle (DTN). A BDTN model has been designed and subjected to dynamic experimental study. The main results show that: (1) The frequency spectrums of the dynamic pressures are different between each thrust vector state. (2) The variation rates of dynamic vector of the new BDTN can reach as high as 50 deg/s, 40 deg/s, and 34 deg/s under nozzle pressure ratio NPR = 3, 5, and 10, separately. (3)The dynamic hysteresis time is less than 1 ms.
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      Dynamic Experimental Investigations of a Bypass Dual Throat Nozzle

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/158021
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorGu, Rui
    contributor authorXu, Jinglei
    date accessioned2017-05-09T01:18:07Z
    date available2017-05-09T01:18:07Z
    date issued2015
    identifier issn1528-8919
    identifier othergtp_137_08_084501.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/158021
    description abstractThe bypass dual throat nozzle (BDTN) does not consume any secondary injection from the other part of the engine, while it can produce steady and efficient vectoring deflection similar to the conventional dual throat nozzle (DTN). A BDTN model has been designed and subjected to dynamic experimental study. The main results show that: (1) The frequency spectrums of the dynamic pressures are different between each thrust vector state. (2) The variation rates of dynamic vector of the new BDTN can reach as high as 50 deg/s, 40 deg/s, and 34 deg/s under nozzle pressure ratio NPR = 3, 5, and 10, separately. (3)The dynamic hysteresis time is less than 1 ms.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDynamic Experimental Investigations of a Bypass Dual Throat Nozzle
    typeJournal Paper
    journal volume137
    journal issue8
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4029391
    journal fristpage84501
    journal lastpage84501
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 008
    contenttypeFulltext
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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