A rotating wind tunnel balance used to study the behavior of aircraft flying at steep angles of attack is described. A particular study carried out on a model of a Mirage type fighter plane, characterized by its delta wing design, is reported on. Measurement signal acquisition and processing are covered. Flight characteristics for both the model stationary and in motion were defined and the significance of these data is discussed.


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    Titel :

    First Results Obtained with a Rotating Construction Premiers Resultats Obtenus Par la Societe Avions Marcel Dassault-Breguet Aviation sur le Montage Tournant de l'Institut de Mecanique des Fluides, Lille


    Beteiligte:
    C. Couedor (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    22 pages



    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch