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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Unsteady Aerodynamics of Moving Control Surfaces at the Airbus Wing


    Contributors:
    G. Anders (author)

    Publication date :

    1984


    Size :

    23 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English