The use of aeroelastic model tests in aircraft design is outlined. Aeroelastic models are economical for the development and testing of novel active-control technologies and measuring methods for aircraft vibration tests. The linearized dynamic calculation model of a flying elastic aircraft was realized in a wind tunnel using aeroelastic models. The validity domain of an aeroelastic model was substantially extended in a cryogenic wind tunnel.


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    Title :

    Aeroelastische Modelle in der Flugzeugentwicklung (Aeroelastic Models in Aircraft Design)


    Contributors:
    H. Hoenlinger (author) / O. Sensburg (author)

    Publication date :

    1986


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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