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 derivates. The natural dynamic behavior of the model was changed in order to simulate different aircraft in different missions.


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    Title :

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


    Contributors:
    H. Subke (author)

    Publication date :

    1983


    Size :

    156 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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