YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    Search 
    •   YE&T Library
    • Search
    •   YE&T Library
    • Search
    • 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.

    Search

    Show Advanced FiltersHide Advanced Filters

    Filters

    Use filters to refine the search results.

    Now showing items 1-3 of 3

    • Relevance
    • Title Asc
    • Title Desc
    • Year Asc
    • Year Desc
    • 5
    • 10
    • 20
    • 40
    • 60
    • 80
    • 100
  • Export
    • CSV
    • RIS
    • Sort Options:
    • Relevance
    • Title Asc
    • Title Desc
    • Issue Date Asc
    • Issue Date Desc
    • Results Per Page:
    • 5
    • 10
    • 20
    • 40
    • 60
    • 80
    • 100

    Effect of Reynolds Number and Periodic Unsteady Wake Flow Condition on Boundary Layer Development, Separation, and Intermittency Behavior Along the Suction Surface of a Low Pressure Turbine Blade 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 001:;page 92
    Author(s): M. T. Schobeiri; David E. Ashpis; B. Öztürk
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper experimentally studies the effects of periodic unsteady wake flow and Reynolds number on boundary layer development, separation, reattachment, and the intermittency behavior along the ...
    Request PDF

    On the Physics of Flow Separation Along a Low Pressure Turbine Blade Under Unsteady Flow Conditions 

    Source: Journal of Fluids Engineering:;2005:;volume( 127 ):;issue: 003:;page 503
    Author(s): Meinhard T. Schobeiri; David E. Ashpis; Burak Öztürk
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present study, which is the first of a series of investigations dealing with specific issues of low pressure turbine (LPT) boundary layer aerodynamics, is aimed at providing detailed unsteady ...
    Request PDF

    Predictions of Separated and Transitional Boundary Layers Under Low-Pressure Turbine Airfoil Conditions Using an Intermittency Transport Equation 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 003:;page 455
    Author(s): Y. B. Suzen; Senior Engineer Associate; Lennart S. Hultgren; Aerospace Engineer; David E. Ashpis; Aerospace Engineer; P. G. Huang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new transport equation for the intermittency factor was proposed to predict separated and transitional boundary layers under low-pressure turbine airfoil conditions. The intermittent behavior of ...
    Request PDF
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     

    Author

    ... View More

    Publisher

    Year

    Type

    Content Type

    Publication Title

    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian