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 1-10 of 14

    • 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

    Fluctuating Thermal Field in the Near-Hole Region for Film Cooling Flows 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 001:;page 86
    Author(s): A. Kohli; D. G. Bogard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The film cooling flow field is the result of a highly complex interaction between the film cooling jets and the mainstream. Understanding this interaction is important in order to explain the ...
    Request PDF

    Adiabatic Effectiveness, Thermal Fields, and Velocity Fields for Film Cooling With Large Angle Injection 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 002:;page 352
    Author(s): A. Kohli; D. G. Bogard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The film cooling performance and velocity field were investigated for discrete round holes inclined at an injection angle of 55 deg. Results are compared to typical round film cooling holes, ...
    Request PDF

    Effects of Very High Free-Stream Turbulence on the Jet–Mainstream Interaction in a Film Cooling Flow 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 004:;page 785
    Author(s): A. Kohli; D. G. Bogard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Dispersion of coolant jets in a film cooling flow field is the result of a highly complex interaction between the film cooling jets and the mainstream. Understanding this complex interaction, ...
    Request PDF

    Enhanced Heat Transfer and Shear Stress Due to High Free-Stream Turbulence 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 003:;page 418
    Author(s): K. A. Thole; D. G. Bogard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Surface heat transfer and skin friction enhancements, as a result of free-stream turbulence levels between 10 percent < Tu > 20 percent, have been measured and compared in terms of ...
    Request PDF

    High Freestream Turbulence Effects on Turbulent Boundary Layers 

    Source: Journal of Fluids Engineering:;1996:;volume( 118 ):;issue: 002:;page 276
    Author(s): K. A. Thole; D. G. Bogard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: High freestream turbulence levels significantly alter the characteristics of turbulent boundary layers. Numerous studies have been conducted with freestreams having turbulence levels of 7 percent ...
    Request PDF

    Characterization and Laboratory Simulation of Turbine Airfoil Surface Roughness and Associated Heat Transfer 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 002:;page 337
    Author(s): D. G. Bogard; M. Tabbita; D. L. Schmidt
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The physical characteristics of surface roughness observed on first-stage high-pressure turbine vanes that had been in service for a long period were investigated in this study. Profilometry ...
    Request PDF

    Film Cooling With Compound Angle Holes: Heat Transfer 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 004:;page 800
    Author(s): B. Sen; D. L. Schmidt; D. G. Bogard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Heat transfer coefficients have been measured for film cooling injection from a single row of holes laterally directed with a compound angle of 60 deg. Two hole configurations were tested, ...
    Request PDF

    Film Cooling With Compound Angle Holes: Adiabatic Effectiveness 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 004:;page 807
    Author(s): D. L. Schmidt; B. Sen; D. G. Bogard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Film cooling effectiveness was studied experimentally in a flat plate test facility with zero pressure gradient using a single row of inclined holes, which injected high-density, cryogenically ...
    Request PDF

    Hydrodynamic Measurements of Jets in Crossflow for Gas Turbine Film Cooling Applications 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 002:;page 139
    Author(s): J. R. Pietrzyk; D. G. Bogard; M. E. Crawford
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the results of a detailed hydrodynamic study of a row of inclined jets issuing into a crossflow. Laser-Doppler anemometry was used to measure the vertical and streamwise ...
    Request PDF

    Effects of Density Ratio on the Hydrodynamics of Film Cooling 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003:;page 437
    Author(s): J. R. Pietrzyk; D. G. Bogard; M. E. Crawford
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the results of a detailed hydrodynamic study of a row of inclined jets issuing into a crossflow with a density ratio of injectant to free stream of 2. Laser-Doppler ...
    Request PDF
    • 1
    • 2
    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