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Effect of inlet turbulence on compressible flow through the tip-section turbine blade cascade with supersonic inlet

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F18%3AN0000095" target="_blank" >RIV/00010669:_____/18:N0000095 - isvavai.cz</a>

  • Alternative codes found

    RIV/61388998:_____/18:00490790

  • Result on the web

    <a href="https://www.matec-conferences.org/articles/matecconf/pdf/2018/27/matecconf_xxi.aeanmifmae-2018_02007.pdf" target="_blank" >https://www.matec-conferences.org/articles/matecconf/pdf/2018/27/matecconf_xxi.aeanmifmae-2018_02007.pdf</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1051/matecconf/201816802007" target="_blank" >10.1051/matecconf/201816802007</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Effect of inlet turbulence on compressible flow through the tip-section turbine blade cascade with supersonic inlet

  • Original language description

    The contribution deals with the numerical simulation of 2D compressible flow though the tip-section turbine blade cascade with the supersonic inlet boundary conditions. The simulation was carried out by the in-house numerical code using the explicit algebraic Reynolds stress model completed by the bypass transition model with the algebraic equation for the intermittency coefficient. The γ-Re model implemented in the commercial code Fluent was used for the comparison. Predictions carried out for the nominal conditions were focused on the effect of inlet free-stream turbulence on the flow structure in the blade cascade under supersonic inlet conditions. Numerical results were compared with experimental data.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20303 - Thermodynamics

Result continuities

  • Project

    <a href="/en/project/TH02020057" target="_blank" >TH02020057: Turbine profile cascades for supersonic flow fields</a><br>

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2018

  • Confidentiality

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

Data specific for result type

  • Article name in the collection

    MATEC Web of Conferences, 168, art. no. 02007

  • ISBN

  • ISSN

    2261236X

  • e-ISSN

  • Number of pages

    9

  • Pages from-to

    nestrankovano

  • Publisher name

    EDP Sciences

  • Place of publication

    neuveden

  • Event location

    Rajecké Teplice, Slovakia

  • Event date

    Apr 25, 2018

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article

    000454319000010