YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Fluids Engineering
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Fluids Engineering
    • 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

    An Experimental Investigation of Cavitation Inception and Development on a Two-Dimensional Eppler Hydrofoil

    Source: Journal of Fluids Engineering:;2000:;volume( 122 ):;issue: 001::page 164
    Author:
    J.-A. Astolfi
    ,
    I. Cid Tomas
    ,
    P. Dorange
    ,
    Ph.D. Student
    ,
    J.-Y. Billard
    ,
    Senior Researcher
    ,
    Head of LHEN
    DOI: 10.1115/1.483239
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Cavitation inception and development on a two-dimensional foil with an Eppler E817 cross section issued from an inverse calculus have been experimentally investigated. The foil is theoretically designed to have a wide cavitation-free bucket allowing a large range of cavitation-free angle of incidence (Eppler, R., 1990, Airfoil Design and Data, Springer-Verlag, Berlin). The inception cavitation numbers, the noise level, the velocity distribution, the minimum pressure coefficient, the cavitation patterns (bubble, leading edge “band type” cavitation, attached sheet cavity), together with the sheet cavity length have been experimentally determined. Effects on the velocity field have been studied too with a slightly developed cavitation. For angles of incidence larger than 1 deg, a great difference exists between the inception cavitation number and the theoretical minimum pressure coefficient. However it is in agreement with the measured one obtained from velocity measurements (for 0 deg<α<6 deg). Discrepancy between theory and experiment on scale models is generally attributed to a flow separation at the leading edge. Although there are some indications of a separated flow at the leading edge, the velocity measurements do not show reverse flow with clearly detected negative velocities excepted for a large angle of incidence equal to 10 deg. Concerning sheet cavity development, the length cavity is found to scale as [σ/2(α−αi(σ))]−m with m close to 2, for length cavities that do not exceed half the foil chord and for σ/2(α−αi(σ)) larger than about 30. [S0098-2202(00)00201-7]
    keyword(s): Pressure , Flow (Dynamics) , Cavitation , Cavities , Hydrofoil , Bubbles AND Chords (Trusses) ,
    • Download: (462.0Kb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      An Experimental Investigation of Cavitation Inception and Development on a Two-Dimensional Eppler Hydrofoil

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/123926
    Collections
    • Journal of Fluids Engineering

    Show full item record

    contributor authorJ.-A. Astolfi
    contributor authorI. Cid Tomas
    contributor authorP. Dorange
    contributor authorPh.D. Student
    contributor authorJ.-Y. Billard
    contributor authorSenior Researcher
    contributor authorHead of LHEN
    date accessioned2017-05-09T00:02:47Z
    date available2017-05-09T00:02:47Z
    date copyrightMarch, 2000
    date issued2000
    identifier issn0098-2202
    identifier otherJFEGA4-27148#164_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123926
    description abstractCavitation inception and development on a two-dimensional foil with an Eppler E817 cross section issued from an inverse calculus have been experimentally investigated. The foil is theoretically designed to have a wide cavitation-free bucket allowing a large range of cavitation-free angle of incidence (Eppler, R., 1990, Airfoil Design and Data, Springer-Verlag, Berlin). The inception cavitation numbers, the noise level, the velocity distribution, the minimum pressure coefficient, the cavitation patterns (bubble, leading edge “band type” cavitation, attached sheet cavity), together with the sheet cavity length have been experimentally determined. Effects on the velocity field have been studied too with a slightly developed cavitation. For angles of incidence larger than 1 deg, a great difference exists between the inception cavitation number and the theoretical minimum pressure coefficient. However it is in agreement with the measured one obtained from velocity measurements (for 0 deg<α<6 deg). Discrepancy between theory and experiment on scale models is generally attributed to a flow separation at the leading edge. Although there are some indications of a separated flow at the leading edge, the velocity measurements do not show reverse flow with clearly detected negative velocities excepted for a large angle of incidence equal to 10 deg. Concerning sheet cavity development, the length cavity is found to scale as [σ/2(α−αi(σ))]−m with m close to 2, for length cavities that do not exceed half the foil chord and for σ/2(α−αi(σ)) larger than about 30. [S0098-2202(00)00201-7]
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Experimental Investigation of Cavitation Inception and Development on a Two-Dimensional Eppler Hydrofoil
    typeJournal Paper
    journal volume122
    journal issue1
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.483239
    journal fristpage164
    journal lastpage173
    identifier eissn1528-901X
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsCavitation
    keywordsCavities
    keywordsHydrofoil
    keywordsBubbles AND Chords (Trusses)
    treeJournal of Fluids Engineering:;2000:;volume( 122 ):;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