Introduction of new technologies to aerospace applications necessarily requires methods of non-destructive testing suitable to evaluate structural integrity. This important task also occurred when it was decided to develop and manufacture a large Fin-Box-Demonstrator equivalent to a fighter aircraft tail equipped with surface bonded piezoceramic actuators between DaimlerChrysler Aerospace - Military Aircraft Division and DaimlerChrysler Research and Technology. The objective of this project is to prove that structural vibrations of a fighter aircraft tail fin due to buffeting can be damped actively by means of surface bonded piezoceramic actuators.


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    Titel :

    Nondestructive testing of surface-bonded piezoelectric patch actuators


    Beteiligte:
    Duerr, Johannes K. (Autor:in) / Krohn, Nils (Autor:in) / Nixdorf, Klaus (Autor:in) / Luetze, Steffen (Autor:in) / Herold-Schmidt, Ursula (Autor:in) / Busse, Gerhard (Autor:in)

    Kongress:

    Smart Structures and Materials 1999: Industrial and Commercial Applications of Smart Structures Technologies ; 1999 ; Newport Beach,CA,USA


    Erschienen in:

    Erscheinungsdatum :

    09.07.1999





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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