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    Affordable Nacelle Technologies for Future Turbofans

    Source: Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 002::page 236
    Author:
    C. J. Smith
    DOI: 10.1115/1.2816582
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Costs are playing an ever-increasing role in determining what the next generation of aircraft and engines will be. In addition to deciding to what extent wing/engine integration or drag-reducing laminar flow technologies can be employed, etc., the economic impact on both aircraft operation and engines launch and development costs must be evaluated. SFC or fuel burn advantages are no longer dominant to the extent they used to be and for some apparently promising technology concepts the cost disadvantages outweigh the aerodynamic advantages when both effects are transposed into aircraft direct operating costs. In addition, a simple metric has been evolved to rank different technology concepts and prioritize them in order to help determine the most deserving technologies for scarce development funds.
    keyword(s): Fuels , Engines , Drag (Fluid dynamics) , Laminar flow , Aircraft , Wings AND Turbofans ,
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      Affordable Nacelle Technologies for Future Turbofans

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    http://yetl.yabesh.ir/yetl1/handle/yetl/116927
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    contributor authorC. J. Smith
    date accessioned2017-05-08T23:50:06Z
    date available2017-05-08T23:50:06Z
    date copyrightApril, 1996
    date issued1996
    identifier issn1528-8919
    identifier otherJETPEZ-26751#236_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116927
    description abstractCosts are playing an ever-increasing role in determining what the next generation of aircraft and engines will be. In addition to deciding to what extent wing/engine integration or drag-reducing laminar flow technologies can be employed, etc., the economic impact on both aircraft operation and engines launch and development costs must be evaluated. SFC or fuel burn advantages are no longer dominant to the extent they used to be and for some apparently promising technology concepts the cost disadvantages outweigh the aerodynamic advantages when both effects are transposed into aircraft direct operating costs. In addition, a simple metric has been evolved to rank different technology concepts and prioritize them in order to help determine the most deserving technologies for scarce development funds.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAffordable Nacelle Technologies for Future Turbofans
    typeJournal Paper
    journal volume118
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2816582
    journal fristpage236
    journal lastpage239
    identifier eissn0742-4795
    keywordsFuels
    keywordsEngines
    keywordsDrag (Fluid dynamics)
    keywordsLaminar flow
    keywordsAircraft
    keywordsWings AND Turbofans
    treeJournal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 002
    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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