YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    • 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.

    Archive

    Highly Aggressive Intercompressor Duct With Active Flow Control: Numerical Validation of Pulsed Jet Actuators With Unsteady Simulations

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:006::page 1333
    Author:
    Fritz, Stefan
    ,
    Koppers, Felix
    ,
    Hergt, Alexander
    ,
    Bresemann, David
    ,
    Eck, Mario
    ,
    Peitsch, Dieter
    ,
    Möller, Felix M.
    ,
    Rückert, Roland
    DOI: 10.1115/1.4070230
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. The application of active flow control (AFC) methods in an intercompressor duct (ICD) offers the possibility of further length reduction while suppressing separations. In particular, pulsed jet actuators (PJAs) are advantageous because the pulsation enhances mixing processes. However, the PJAs require fluid that has already been compressed by the downstream high-pressure compressor. Therefore, injecting this high-momentum fluid from a downstream component makes this approach very expensive. Consequently, a highly optimized design is required to achieve the maximum separation suppression while minimizing the external energy. However, the numerical optimization requires steady simulations to find an optimum design in manageable time scales. Therefore, this study helps in understanding if any aspects of unsteadiness are neglected by optimizing the PJA implementation with steady methods. Furthermore, the influence of the steady-state assumption in the optimization is quantified. The influence of the unsteadiness of the PJA is investigated by comparing steady and unsteady simulations. The unsteady simulations include unsteady Reynolds-averaged Navier–Stokes and delayed detached-eddy simulation. The numerical simulations are validated against experimental data obtained at the TU Berlin ICD test rig. After evaluating the different approaches, a conclusion is drawn on how unsteady flow control methods can be efficiently optimized. Consequently, the study shows that all the methods investigated have their advantages and disadvantages. Their use must be carefully selected according to the objective of the investigation.
    • Download: (1.574Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Statistics

      Highly Aggressive Intercompressor Duct With Active Flow Control: Numerical Validation of Pulsed Jet Actuators With Unsteady Simulations

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/4316924
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorFritz, Stefan
    contributor authorKoppers, Felix
    contributor authorHergt, Alexander
    contributor authorBresemann, David
    contributor authorEck, Mario
    contributor authorPeitsch, Dieter
    contributor authorMöller, Felix M.
    contributor authorRückert, Roland
    date accessioned2026-08-23T08:42:28Z
    date available2026-08-23T08:42:28Z
    date copyright2026/06/01
    date issued2026
    identifier issn0889-504X
    identifier otherturbo-25-1217.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4316924
    description abstractAbstract. The application of active flow control (AFC) methods in an intercompressor duct (ICD) offers the possibility of further length reduction while suppressing separations. In particular, pulsed jet actuators (PJAs) are advantageous because the pulsation enhances mixing processes. However, the PJAs require fluid that has already been compressed by the downstream high-pressure compressor. Therefore, injecting this high-momentum fluid from a downstream component makes this approach very expensive. Consequently, a highly optimized design is required to achieve the maximum separation suppression while minimizing the external energy. However, the numerical optimization requires steady simulations to find an optimum design in manageable time scales. Therefore, this study helps in understanding if any aspects of unsteadiness are neglected by optimizing the PJA implementation with steady methods. Furthermore, the influence of the steady-state assumption in the optimization is quantified. The influence of the unsteadiness of the PJA is investigated by comparing steady and unsteady simulations. The unsteady simulations include unsteady Reynolds-averaged Navier–Stokes and delayed detached-eddy simulation. The numerical simulations are validated against experimental data obtained at the TU Berlin ICD test rig. After evaluating the different approaches, a conclusion is drawn on how unsteady flow control methods can be efficiently optimized. Consequently, the study shows that all the methods investigated have their advantages and disadvantages. Their use must be carefully selected according to the objective of the investigation.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHighly Aggressive Intercompressor Duct With Active Flow Control: Numerical Validation of Pulsed Jet Actuators With Unsteady Simulations
    typeJournal Paper
    journal volume148
    journal issue6
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4070230
    journal fristpage1333
    journal lastpage1350
    page18
    treeJournal of Turbomachinery:;2026:;volume( 148 ):;issue:006
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian