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    Perspective: Unsteady Wing Theory—The Kármán/Sears Legacy

    Source: Journal of Fluids Engineering:;1993:;volume( 115 ):;issue: 004::page 548
    Author:
    J. E. McCune
    ,
    T. S. Tavares
    DOI: 10.1115/1.2910179
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aerodynamic analysis of wings and their vortex wakes is discussed from a perspective of its relation to the 1938 work of Kármán and Sears. The key concepts from this early paper on the analysis of airfoils in small amplitude unsteady motion are reviewed. These concepts are then used as a point of departure for developing techniques for calculating and interpreting the aerodynamic characteristics of both airfoils in large amplitude motion with deforming vortex wakes, and maneuvering low-aspect-ratio wings with leading-edge separation. Calculated examples are presented for this extended set of applications, and are compared to related analyses and experiments.
    keyword(s): Wings , Airfoils , Motion , Wakes , Vortices AND Separation (Technology) ,
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      Perspective: Unsteady Wing Theory—The Kármán/Sears Legacy

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/112065
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    contributor authorJ. E. McCune
    contributor authorT. S. Tavares
    date accessioned2017-05-08T23:41:35Z
    date available2017-05-08T23:41:35Z
    date copyrightDecember, 1993
    date issued1993
    identifier issn0098-2202
    identifier otherJFEGA4-27080#548_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112065
    description abstractThe aerodynamic analysis of wings and their vortex wakes is discussed from a perspective of its relation to the 1938 work of Kármán and Sears. The key concepts from this early paper on the analysis of airfoils in small amplitude unsteady motion are reviewed. These concepts are then used as a point of departure for developing techniques for calculating and interpreting the aerodynamic characteristics of both airfoils in large amplitude motion with deforming vortex wakes, and maneuvering low-aspect-ratio wings with leading-edge separation. Calculated examples are presented for this extended set of applications, and are compared to related analyses and experiments.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePerspective: Unsteady Wing Theory—The Kármán/Sears Legacy
    typeJournal Paper
    journal volume115
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.2910179
    journal fristpage548
    journal lastpage560
    identifier eissn1528-901X
    keywordsWings
    keywordsAirfoils
    keywordsMotion
    keywordsWakes
    keywordsVortices AND Separation (Technology)
    treeJournal of Fluids Engineering:;1993:;volume( 115 ):;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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