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 1-4 of 4

    • 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

    Aeroderivative Mechanical Drive Gas Turbines: The Design of Intermediate Pressure Turbines 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 08:;page 81007
    Author(s): Del Greco, Alberto Scotti; Michelassi, Vittorio; Francini, Stefano; Di Benedetto, Daniele; Manoharan, Mahendran
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Gas turbines engine designers are leaning toward aircraft engine architectures due to their footprint, weight, and performance advantages. Such engines need some modifications to both the combustion system, to comply with ...
    Request PDF

    Aeroderivative Mechanical Drive Gas Turbines: The Design of Intermediate Pressure Turbines 

    Source: Journal of Turbomachinery:;2019:;volume 141:;issue 008:;page 81007
    Author(s): Del Greco, Alberto Scotti; Michelassi, Vittorio; Francini, Stefano; Di Benedetto, Daniele; Manoharan, Mahendran
    Publisher: American Society of Mechanical Engineers (ASME)
    Abstract: Gas turbines engine designers are leaning toward aircraft engine architectures due to their footprint, weight, and performance advantages. Such engines need some modifications to both the combustion system, to comply with ...
    Request PDF

    Axial Compressor Transonic Rotor Shock Interaction With Upstream Stator Row 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 009:;page 91011-1
    Author(s): Michelassi, Vittorio; Burberi, Corrado; Koyyalamudi, Satish; Lorusso, Salvatore; Del Greco, Alberto Scotti
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Modern multistage axial compressors are designed for high aerodynamic loading and wide range with front stages rotor inlet relative Mach number above one over a large portion of span. Rotor shock waves propagate and reflect ...
    Request PDF

    Introduction of Circumferentially Nonuniform Variable Guide Vanes in the Inlet Plenum of a Centrifugal Compressor for Minimum Losses and Flow Distortion 

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 009:;page 91008
    Author(s): Sezal, Ismail; Chen, Nan; Aalburg, Christian; Gadamsetty, Rajesh Kumar V.; Erhard, Wolfgang; Del Greco, Alberto Scotti; Tapinassi, Libero; Lang, Matthias
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the oil and gas industry, large variations in flow rates are often encountered, which require compression trains with a wide operating range. If the stable operating range at constant speed is insufficient, variable ...
    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