Effects of an Oscillating Flap on the Main Airfoil Unsteady Lift in Grid Turbulence

Herricos Stapountzis*, Athanasios Barlas, Georgios Papageorgiou, Athanasios Patsiouras

*Corresponding author for this work

    Research output: Chapter in Book/Report/Conference proceedingArticle in proceedingsResearch

    Abstract

    A wing of NACA 0015 profile and Aspect Ratio 2.4 fitted with a Trailing Edge Flap was tested in a wind tunnel for both smooth and turbulent flow conditions at a Re number 108000. The unsteady lift on the wing was measured with and without the flap. Two types of flap excitation were tried: One was of the “open loop” type in which the flap was subjected to sinusoidal pitching oscillations while the wing was set to a constant angle of attack. In the second, “closed loop” mode, the excitation signal fed into the flap originated from the unsteady lift of the wing itself. The phase lag between those signals was changed and it was found that it played a significant role in the suppression of the main wing unsteady lift.
    Original languageEnglish
    Title of host publicationAdvances in Critical Flow Dynamics Involving Moving/Deformable Structures with Design Applications
    EditorsMarianna Braza , Kerry Hourigan , Michael Triantafyllou
    Number of pages11
    PublisherSpringer
    Publication date2021
    Pages493-503
    ISBN (Print)978-3-030-55593-1
    ISBN (Electronic)978-3-030-55594-8
    DOIs
    Publication statusPublished - 2021
    EventIUTAM Symposium on Critical Flow Dynamics involving Moving/Deformable Structures with Design applications - Satorini, Greece
    Duration: 18 Jun 201822 Jun 2018

    Conference

    ConferenceIUTAM Symposium on Critical Flow Dynamics involving Moving/Deformable Structures with Design applications
    Country/TerritoryGreece
    CitySatorini
    Period18/06/201822/06/2018
    SeriesNotes on Numerical Fluid Mechanics and Multidisciplinary Design
    Volume147
    ISSN1612-2909

    Keywords

    • Trailing edge flap
    • Wind turbine load alleviation
    • Smart blades
    • Unsteady aerodynamics
    • Active flow control

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