A wind tunnel test of a dynamically scaled aircraft model equipped with sensors and actuators is presented. The dynamic response was compared with the result of a computer simulation. A good correlation is obtained after adjustment of the dynamic derivatives. The natural dynamic behavior of the model was changed in order to simulate different aircraft in different missions.


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    Titel :

    Flight-Mechanics Test with a Restricted Flying Aircraft Model in a Wind Tunnel


    Beteiligte:
    H. Subke (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    151 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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