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    Aerodynamic Performance of a Scale-Model, Counterrotating Unducted Fan

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 004::page 579
    Author:
    T. J. Sullivan
    DOI: 10.1115/1.2927696
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aerodynamic performance of a scale-model, counterrotating unducted fan has been determined and the results are discussed herein. Experimental investigations were conducted using the scale-model propulsor simulator and uniquely shaped fan blades designed by the General Electric Company under contract to NASA. The blades, designed for a high disk loading at Mach 0.72, 35,000 ft altitude max climb condition, are aft-mounted on the simulator in a “pusher” configuration. Data are compared with analytical predictions at the design point and show good agreement.
    keyword(s): Design , Disks AND Blades ,
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      Aerodynamic Performance of a Scale-Model, Counterrotating Unducted Fan

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    http://yetl.yabesh.ir/yetl1/handle/yetl/107683
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    contributor authorT. J. Sullivan
    date accessioned2017-05-08T23:33:59Z
    date available2017-05-08T23:33:59Z
    date copyrightOctober, 1990
    date issued1990
    identifier issn0889-504X
    identifier otherJOTUEI-28606#579_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107683
    description abstractThe aerodynamic performance of a scale-model, counterrotating unducted fan has been determined and the results are discussed herein. Experimental investigations were conducted using the scale-model propulsor simulator and uniquely shaped fan blades designed by the General Electric Company under contract to NASA. The blades, designed for a high disk loading at Mach 0.72, 35,000 ft altitude max climb condition, are aft-mounted on the simulator in a “pusher” configuration. Data are compared with analytical predictions at the design point and show good agreement.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAerodynamic Performance of a Scale-Model, Counterrotating Unducted Fan
    typeJournal Paper
    journal volume112
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927696
    journal fristpage579
    journal lastpage586
    identifier eissn1528-8900
    keywordsDesign
    keywordsDisks AND Blades
    treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 004
    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
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