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 12

    • 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

    Influence of the Hole Length-to-Diameter Ratio on Film Cooling With Cylindrical Holes 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 002:;page 209
    Author(s): E. Lutum; B. V. Johnson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Film cooling experiments were conducted to investigate the effects of coolant hole length-to-diameter ratio on the film cooling effectiveness. The results from these experiments offer an explanation ...
    Request PDF

    Statistical Characteristics of Velocity, Concentration, Mass Transport, and Momentum Transport for Coaxial Jet Mixing in a Confined Duct 

    Source: Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 001:;page 121
    Author(s): B. V. Johnson; J. C. Bennett
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental study of mixing downstream of coaxial jets discharging into an expanded circular duct was conducted to obtain data for the evaluation and improvement of turbulent transport models ...
    Request PDF

    Heat Transfer in Rotating Serpentine Passages With Smooth Walls 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 003:;page 321
    Author(s): J. H. Wagner; F. C. Kopper; B. V. Johnson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments were conducted to determine the effects of buoyancy and Coriolis forces on heat transfer in turbine blade internal coolant passages. The experiments were conducted with a large-scale, ...
    Request PDF

    Heat Transfer in Rotating Passages With Smooth Walls and Radial Outward Flow 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 001:;page 42
    Author(s): J. H. Wagner; T. J. Hajek; B. V. Johnson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments were conducted to determine the effects of rotation on heat transfer in turbine blade internal coolant passages. The experiments were conducted with a smooth wall, large-scale heat ...
    Request PDF

    Aerodynamic and Torque Characteristics of Enclosed Co/Counterrotating Disks 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 001:;page 67
    Author(s): W. A. Daniels; B. V. Johnson; D. J. Graber
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments were conducted to determine the aerodynamic and torque characteristics of adjacent rotating disks enclosed in a shroud. These experiments were performed to obtain an extended data ...
    Request PDF

    Cold Flow and Combustion Experiments With a New Burner Air Distribution Concept 

    Source: Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 002:;page 370
    Author(s): B. V. Johnson; S. J. Markowski; H. M. Craig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments were conducted with a JT8D-engine sized can combustor modified such that all the combustion and dilution air entered through the burner front face from a single plenum through ...
    Request PDF

    Comparison of Performance of Supersonic Blading in Cascade and in Compressor Rotors 

    Source: Journal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 001:;page 42
    Author(s): A. A. Mikolajczak; B. V. Johnson; A. L. Morris
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Reduction of engine weight and engine specific fuel consumption is a continuing goa of jet engine designers. An attractive approach is through the development of efficient, high-tip speed ...
    Request PDF

    Rim Seal Experiments and Analysis for Turbine Applications 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 002:;page 426
    Author(s): W. A. Daniels; D. J. Graber; R. J. Martin; B. V. Johnson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation was conducted to determine the sealing effectiveness and the aerodynamic characteristics of four rim seal models for a number of flow conditions. The experiments ...
    Request PDF

    Heat Transfer in Rotating Serpentine Passages With Trips Normal to the Flow 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 004:;page 847
    Author(s): J. H. Wagner; R. A. Graziani; F. C. Yeh; B. V. Johnson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments were conducted to determine the effects of buoyancy and Coriolis forces on heat transfer in turbine blade internal coolant passages. The experiments were conducted with a large-scale, ...
    Request PDF

    Compressor Drum Aerodynamic Experiments and Analysis With Coolant Injected at Selected Locations 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 002:;page 272
    Author(s): B. V. Johnson; E. J. Kawecki; R. J. Martin; W. A. Daniels
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments were conducted to determine the pressure distributions within a multicavity compressor drum model for two coolant injection locations and a range of flow conditions. Flow was injected ...
    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