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 1-9 of 9

    • 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

    Discharge Coefficient of Turbine Cooling Holes: A Review 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 002:;page 314
    Author(s): N. Hay; D. Lampard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Published information on the discharge coefficient of film cooling holes is classified in terms of the hole geometry, the external flow conditions at inlet and outlet, and the method of ...
    Request PDF

    The Flow and Film Cooling Effectiveness Following Injection through a Row of Holes 

    Source: Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 003:;page 584
    Author(s): N. W. Foster; D. Lampard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Using a mass transfer technique, detailed studies have been made of the effectiveness and flow downstream of a row of holes in the flat floor of a wind tunnel. The effects of variation of ...
    Request PDF

    Effect of Crossflows on the Discharge Coefficient of Film Cooling Holes 

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002:;page 243
    Author(s): N. Hay; D. Lampard; S. Benmansour
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The strongest flow parameter governing the film cooling effectiveness provided by a row of holes is the blowing rate. Precise setting of the blowing rate at the design stage requires accurate ...
    Request PDF

    Effects of the Condition of the Approach Boundary Layer and of Mainstream Pressure Gradients on the Heat Transfer Coefficient on Film-Cooled Surfaces 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 001:;page 99
    Author(s): N. Hay; D. Lampard; C. L. Saluja
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes an investigation of the sensitivity of the heat transfer coefficient under the film to the state of the approach boundary layer for injection through a row of holes on ...
    Request PDF

    The Effect of Density Ratio on the Heat Transfer Coefficient From a Film-Cooled Flat Plate 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003:;page 444
    Author(s): H. D. Ammari; N. Hay; D. Lampard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of density ratio of cooling films on the heat transfer coefficient on a flat plate is investigated using a heat-mass transfer analogy. The experimental technique employed uses a ...
    Request PDF

    Effect of Acceleration on the Heat Transfer Coefficient on a Film-Cooled Surface 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 003:;page 464
    Author(s): H. D. Ammari; N. Hay; D. Lampard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Results are presented of an experimental investigation into the influence of mainstream acceleration on the heat transfer coefficient downstream of injection through a row of 35 deg holes in a ...
    Request PDF

    Effects of Cooling Films on the Heat Transfer Coefficient on a Flat Plate With Zero Mainstream Pressure Gradient 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 001:;page 105
    Author(s): N. Hay; D. Lampard; C. L. Saluja
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The influence of injection of cooling films through a row of holes on the heat transfer coefficient on a flat plate is investigated for a range of mass flux ratio using a heat-mass transfer ...
    Request PDF

    The Film Cooling Effectiveness of Double Rows of Holes 

    Source: Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 003:;page 601
    Author(s): W. O. Afejuku; N. Hay; D. Lampard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The film cooling effectiveness provided by two rows of holes separated by a range of distances has been studied experimentally using a mass transfer technique. The blowing rates at the two ...
    Request PDF

    Measured Coolant Distributions Downstream of Single and Double Rows of Film Cooling Holes 

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 001:;page 172
    Author(s): W. O. Afejuku; N. Hay; D. Lampard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A mass-transfer technique has been used to investigate experimentally the distribution of coolant from two rows of holes with independently varied blowing rates. Both staggered and in-line ...
    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

    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