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    Some Aerodynamic Problems of Aircraft Engines: Fifty Years After -The 2007 IGTI Scholar Lecture-

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 003::page 31101
    Author:
    Edward M. Greitzer
    DOI: 10.1115/1.2992515
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Problems of high technological interest, for example the development of gas turbine engines, span disciplinary, and often organizational, boundaries. Although collaboration is critical in advancing the technology, it has been less a factor in gas turbine research. In this paper it is proposed that step changes in gas turbine performance can emerge from collaborative research endeavors that involve the development of integrated teams with the needed range of skills. Such teams are an important aspect in product development, but they are less familiar and less subscribed to in the research community. The case histories of two projects are given to illustrate the point: the development of the concept of “smart jet engines” and the Silent Aircraft Initiative. In addition to providing a capability to attack multidisciplinary problems, the way in which collaboration can enhance the research process within a single discipline is also discussed.
    keyword(s): Flow (Dynamics) , Engines , Compressors , Design , Disciplines , Gas turbines , International Gas Turbine Institute , Aircraft , Collaboration , Pressure , Teams , Aircraft engines , Noise (Sound) AND Surges ,
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      Some Aerodynamic Problems of Aircraft Engines: Fifty Years After -The 2007 IGTI Scholar Lecture-

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    http://yetl.yabesh.ir/yetl1/handle/yetl/142153
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    contributor authorEdward M. Greitzer
    date accessioned2017-05-09T00:35:47Z
    date available2017-05-09T00:35:47Z
    date copyrightJuly, 2009
    date issued2009
    identifier issn0889-504X
    identifier otherJOTUEI-28755#031101_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142153
    description abstractProblems of high technological interest, for example the development of gas turbine engines, span disciplinary, and often organizational, boundaries. Although collaboration is critical in advancing the technology, it has been less a factor in gas turbine research. In this paper it is proposed that step changes in gas turbine performance can emerge from collaborative research endeavors that involve the development of integrated teams with the needed range of skills. Such teams are an important aspect in product development, but they are less familiar and less subscribed to in the research community. The case histories of two projects are given to illustrate the point: the development of the concept of “smart jet engines” and the Silent Aircraft Initiative. In addition to providing a capability to attack multidisciplinary problems, the way in which collaboration can enhance the research process within a single discipline is also discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSome Aerodynamic Problems of Aircraft Engines: Fifty Years After -The 2007 IGTI Scholar Lecture-
    typeJournal Paper
    journal volume131
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2992515
    journal fristpage31101
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsEngines
    keywordsCompressors
    keywordsDesign
    keywordsDisciplines
    keywordsGas turbines
    keywordsInternational Gas Turbine Institute
    keywordsAircraft
    keywordsCollaboration
    keywordsPressure
    keywordsTeams
    keywordsAircraft engines
    keywordsNoise (Sound) AND Surges
    treeJournal of Turbomachinery:;2009:;volume( 131 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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