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

    Tradeoff Assessments for Part Load Controlled Cooling Air in Stationary Gas Turbines 

    Source: Journal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 010:;page 0101008-1
    Author(s): Woelki, Dominik; Peitsch, Dieter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The demand for flexible part load operation of stationary gas turbines requires the simultaneous design for sufficient efficiency and lifetime. Both can be addressed by the secondary air system. This paper presents ...
    Request PDF

    An Analysis of the Secondary Flow Around a Tandem Blade Under the Presence of a Tip Gap in a High-Speed Linear Compressor Cascade 

    Source: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 010:;page 101003-1
    Author(s): Konrath, Liesbeth; Peitsch, Dieter; Heinrich, Alexander
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Tandem blades have often been under investigation, experimentally as well as numerically, but most of the studies have been about tandem blade stators without tip gap. This work analyzes the influence of a tip gap on the ...
    Request PDF

    Prestall Instability in Axial Flow Compressors 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 007:;page 071009-1
    Author(s): Eck, Mario; Rückert, Roland; Peitsch, Dieter; Lehmann, Marc
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aim of the present paper is to improve the physical understanding of discrete prestall flow disturbances developing in the tip area of the compressor rotor. For this purpose, a complementary instrumentation was used ...
    Request PDF

    Experimental Investigations on Aeroelastic Stability of Combined Plunge-Pitch Mode Shapes in a Linear Compressor Cascade 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 012:;page 121010-1
    Author(s): Gambel, Julian; Peitsch, Dieter; Schneider, Sabine
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of mode shape and reduced frequency on the flutter stability of a linear low-speed compressor cascade was investigated experimentally, employing the aerodynamic influence coefficient (AIC) approach. This paper ...
    Request PDF

    Transition Mechanisms in Laminar Separated Flow Under Simulated Low Pressure Turbine Aerofoil Conditions 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 001:;page 11007
    Author(s): Dأ¤hnert, Jerrit; Lyko, Christoph; Peitsch, Dieter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Based on detailed experimental work conducted at a low speed test facility, this paper describes the transition process in the presence of a separation bubble with low Reynolds number, low freestream turbulence, and steady ...
    Request PDF

    Forcing of Separation Bubbles by Main Flow Unsteadiness or Pulsed Vortex Generating Jets—A Comparison 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 005:;page 51016
    Author(s): Lyko, Christoph; Dأ¤hnert, Jerrit; Peitsch, Dieter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Low pressure turbines typically operate in the low Reynolds number regime. Depending on the loading of the blade, they may exhibit detached flow with associated reattachment in the rear part of the suction surface. ...
    Request PDF

    Binary Repetitive Model Predictive Active Flow Control Applied to an Annular Compressor Stator Cascade With Periodic Disturbances 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 144 ):;issue: 001:;page 11029-1
    Author(s): Fietzke, Benjamin; Mihalyovics, Jan; King, Rudibert; Peitsch, Dieter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Novel pressure gain combustion concepts invoke periodic flow disturbances in a gas turbine's last compressor stator row. This contribution presents studies of mitigation efforts on the effects of these periodic disturbances ...
    Request PDF

    Numerical Characterization of Prestall Disturbances in a Compressor Stage 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 008:;page 81009-1
    Author(s): de Almeida, Victor Bicalho Civinelli; Tüzüner, Ergin; Eck, Mario; Peitsch, Dieter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Compared to the subject of rotating stall, less attention has been given to prestall flow disturbances in turbomachinery. This is mostly due to the fact that these phenomena, often referred to as Rotating Instabilities, ...
    Request PDF

    A Low-Speed Compressor Test Rig for Flutter Investigations 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 005:;page 51009
    Author(s): Malzacher, Leonie; Geist, Silvio; Motta, Valentina; Peitsch, Dieter; Hennings, Holger
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A test facility for aeroeolastic investigations has been set up at the chair of Aero Engines at the Technische Universität Berlin. The test rig provides data for tool and code validation, and is used for basic aeroelastic ...
    Request PDF

    Experimental Investigation of an Aerodynamically Mistuned Oscillating Compressor Cascade 

    Source: Journal of Turbomachinery:;2019:;volume 141:;issue 007:;page 71012
    Author(s): Malzacher, Leonie; Schwarze, Christopher; Motta, Valentina; Peitsch, Dieter
    Publisher: American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, the effect of aerodynamic mistuning on stability of a compressor cascade is studied. The experiments have been carried out at a low-speed test facility of the Technische Universität Berlin. The test section ...
    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