YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Applied Mechanics
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Applied Mechanics
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    On the Design of Thin Subsonic Airfoils

    Source: Journal of Applied Mechanics:;1979:;volume( 046 ):;issue: 001::page 6
    Author:
    W. C. Chin
    DOI: 10.1115/1.3424530
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The inverse problem, which determines an airfoil geometry given some specified surface pressure, is considered in the subsonic, thin-airfoil limit. The full governing equations are expanded in powers of the thickness ratio and solved to second-order. The two sequential formulations contain free parameters, which are fixed by invoking “Kutta-type” conditions related to trailing edge closure. The correctness of the basic approach is demonstrated by using known classical examples for the simpler first-order problem.
    keyword(s): Design , Airfoils , Pressure , Equations , Geometry , Inverse problems AND Thickness ,
    • Download: (292.4Kb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      On the Design of Thin Subsonic Airfoils

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/91832
    Collections
    • Journal of Applied Mechanics

    Show full item record

    contributor authorW. C. Chin
    date accessioned2017-05-08T23:06:12Z
    date available2017-05-08T23:06:12Z
    date copyrightMarch, 1979
    date issued1979
    identifier issn0021-8936
    identifier otherJAMCAV-26112#6_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/91832
    description abstractThe inverse problem, which determines an airfoil geometry given some specified surface pressure, is considered in the subsonic, thin-airfoil limit. The full governing equations are expanded in powers of the thickness ratio and solved to second-order. The two sequential formulations contain free parameters, which are fixed by invoking “Kutta-type” conditions related to trailing edge closure. The correctness of the basic approach is demonstrated by using known classical examples for the simpler first-order problem.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn the Design of Thin Subsonic Airfoils
    typeJournal Paper
    journal volume46
    journal issue1
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3424530
    journal fristpage6
    journal lastpage8
    identifier eissn1528-9036
    keywordsDesign
    keywordsAirfoils
    keywordsPressure
    keywordsEquations
    keywordsGeometry
    keywordsInverse problems AND Thickness
    treeJournal of Applied Mechanics:;1979:;volume( 046 ):;issue: 001
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian