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 1-8 of 8

    • 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

    Investigation of the Linear Stability Problem of Electrified Jets, Inviscid Analysis 

    Source: Journal of Fluids Engineering:;2012:;volume( 134 ):;issue: 009:;page 91201
    Author(s): Serkan Özgen; Oguz Uzol
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The instability characteristics of a liquid jet discharging from a nozzle into a stagnant gas are investigated using the linear stability theory. Starting with the equations of motion for ...
    Request PDF

    Aerodynamic Loss Characteristics of a Turbine Blade With Trailing Edge Coolant Ejection: Part 2—External Aerodynamics, Total Pressure Losses, and Predictions 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 002:;page 249
    Author(s): Oguz Uzol; Cengiz Camci
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Investigation of the internal fluid mechanic losses for a turbine blade with trailing edge coolant ejection was present in Uzol et al. (2001). The current study is a detailed experimental ...
    Request PDF

    Aerodynamic Loss Characteristics of a Turbine Blade With Trailing Edge Coolant Ejection: Part 1—Effect of Cut-Back Length, Spanwise Rib Spacing, Free-Stream Reynolds Number, and Chordwise Rib Length on Discharge Coefficients 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 002:;page 238
    Author(s): Oguz Uzol; Boris Glezer; Cengiz Camci
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The internal fluid mechanics losses generated between the blade plenum chamber and a reference point located just downstream of the trailing edge are investigated for a turbine blade trailing ...
    Request PDF

    Flow Nonuniformities and Turbulent “Hot Spots” Due to Wake-Blade and Wake-Wake Interactions in a Multi-Stage Turbomachine 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 004:;page 553
    Author(s): Yi-Chih Chow; Oguz Uzol; Joseph Katz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This experimental study provides striking examples of the complex flow and turbulence structure resulting from blade-wake and wake-wake interactions in a multi-stage turbomachine. Particle image ...
    Request PDF

    The Effect of Inlet Guide Vanes Wake Impingement on the Flow Structure and Turbulence Around a Rotor Blade 

    Source: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 001:;page 82
    Author(s): Francesco Soranna; Yi-Chih Chow; Oguz Uzol; Joseph Katz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow structure and turbulence around the leading and trailing edges of a rotor blade operating downstream of a row of inlet guide vanes (IGV) are investigated experimentally. Particle image ...
    Request PDF

    The Effects of Inlet Guide Vane-Wake Impingement on the Boundary Layer and the Near-Wake of a Rotor Blade 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 004:;page 41016
    Author(s): Francesco Soranna; Yi-Chih Chow; Oguz Uzol; Joseph Katz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper examines the response of a rotor blade boundary layer and a rotor near-wake to an impinging wake of an inlet guide vane (IGV) located upstream of the rotor blade. Two-dimensional ...
    Request PDF

    Experimental Investigation of Unsteady Flow Field Within a Two-Stage Axial Turbomachine Using Particle Image Velocimetry 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 004:;page 542
    Author(s): Oguz Uzol; Yi-Chih Chow; Joseph Katz; Charles Meneveau
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed measurements of the flow field within the entire 2nd stage of a two-stage axial turbomachine are performed using particle image velocimetry. The experiments are performed in a facility ...
    Request PDF

    Average Passage Flow Field and Deterministic Stresses in the Tip and Hub Regions of a Multistage Turbomachine 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 004:;page 714
    Author(s): Oguz Uzol; Yi-Chih Chow; Joseph Katz; Charles Meneveau
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper continues our effort to study the dynamics of deterministic stresses in a multistage turbomachine using experimental data. Here we focus on the tip and hub regions and compare them ...
    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