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CFD Analysis of Flow in a Blade Cascade Deformed Due to Forced Torsional Vibration

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F21%3A00547896" target="_blank" >RIV/61388998:_____/21:00547896 - isvavai.cz</a>

  • Alternative codes found

    RIV/46747885:24220/21:00009159

  • Result on the web

    <a href="http://dx.doi.org/10.14311/TPFM.2021.020" target="_blank" >http://dx.doi.org/10.14311/TPFM.2021.020</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.14311/TPFM.2021.020" target="_blank" >10.14311/TPFM.2021.020</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    CFD Analysis of Flow in a Blade Cascade Deformed Due to Forced Torsional Vibration

  • Original language description

    The paper presents a 3D numerical simulation of flow in a blade cascade, whose geometry models the test section of a new experimental facility for blade flutter research. In the experimental setup, the middle blade of the cascade undergoes high-frequency forced sinusoidal pitching oscillation. Due to inertial forces, the slender blade deforms elastically to certain degree. The goal of this study is to assess the influence of the elastic deformation on the flow field. To compute the deformed geometry, a transient structural analysis was performed. In the second part, the CFD model of flow past a 3D blade cascade with deformed and undeformed blade is presented and these two configurations are compared. For the deformed configuration the incidence angle increases along the blade span from -1.8° to -2.7°. However, the Mach number distribution along the span varies less than expected. blade cascade, flutter, turbomachinery, CFD

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20302 - Applied mechanics

Result continuities

  • Project

    <a href="/en/project/GA20-11537S" target="_blank" >GA20-11537S: Experimental research on flutter excitation function in turbomachinery</a><br>

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2021

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Article name in the collection

    Proceedings of Topical Problems of Fluid Mechanics 2021

  • ISBN

    978-80-87012-76-5

  • ISSN

    2336-5781

  • e-ISSN

  • Number of pages

    8

  • Pages from-to

    149-156

  • Publisher name

    Institute of Thermomechanics AS CR, v. v. i.

  • Place of publication

    Prague

  • Event location

    on-line

  • Event date

    Feb 17, 2021

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article

    000853393400018