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Application of synthetic jets actuators in wing-pylon junction area to improve the high lift performances

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F16%3AN0000078" target="_blank" >RIV/00010669:_____/16:N0000078 - isvavai.cz</a>

  • Result on the web

    <a href="https://www.eccomas2016.org/" target="_blank" >https://www.eccomas2016.org/</a>

  • DOI - Digital Object Identifier

Alternative languages

  • Result language

    angličtina

  • Original language name

    Application of synthetic jets actuators in wing-pylon junction area to improve the high lift performances

  • Original language description

    Synthetic jets actuators that produce a zero net mass flow rate have been locally applied at the pylon-wing junction to suppress the high-lift penalties caused by the closely coupled engine integration. The high fidelity numerical simulations utilizing unsteady Reyn-olds-averaged Navier-Stokes have been performed to simulate this problem. A wind tunnel model representing a 2,5D wing with pylon, nacelle and deployed high-lift devices is used for this study. Active flow control applied at the wing-pylon junction area can prevent the larger flow separation on the wing behind the nacelle caused by the slat cutback, increase the lift and to postpone the stall angle by interaction of the vortices from the SJA with vortices dominating this region. The performed unsteady CFD simulations demonstrate the possibility locally affect the flow by utilization of AFC. The geometrical setup of the actuators and the flow variables (blowing coefficient, actuation frequency) have been varied, as well. Two different shapes and positions of the nacelle's strike have also been considered during the simulations. The positive effect of the application of the SJA on maximum lift and stall angle has been observed .

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

    JU - Aeronautics, aerodynamics, aeroplanes

  • OECD FORD branch

Result continuities

  • Project

    <a href="/en/project/7E13056" target="_blank" >7E13056: 2nd Generation Active Wing – Active Flow- Loads & Noise control on next generation wing</a><br>

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Others

  • Publication year

    2016

  • Confidentiality

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

Data specific for result type

  • Article name in the collection

    ECCOMAS Congress 2016 - Proceedings of the 7th European Congress on Computational Methods in Applied Sciences and Engineering, Vol. 3

  • ISBN

    978-618-82844-0-1

  • ISSN

  • e-ISSN

  • Number of pages

    10

  • Pages from-to

    6505-6514

  • Publisher name

    National Technical University of Athens

  • Place of publication

    Greece

  • Event location

    Crete Island, Greece

  • Event date

    Jun 5, 2016

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article