Steady and unsteady tests were carried out in a transonic tunnel on moving control surfaces of the European Airbus wing. A data bank containing the measured configurations of spoilers, flaps, and ailerons is obtained.


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    Titel :

    Unsteady Aerodynamics of Moving Control Surfaces at the Airbus Wing


    Beteiligte:
    G. Anders (Autor:in)

    Erscheinungsdatum :

    1984


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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