The results of an analytical study are presented on the use of boron polyimide filamentary composite material for the purpose of increasing the flutter speed of a simple titanium full depth sandwich wing structure designed for strength. The results clearly demonstrate that selective reinforcement of wing surfaces, using judiciously placed filamentary composites, promises sizable mass savings in the design of advanced aircraft structures.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Selective reinforcement of wing structure for flutter prevention.


    Beteiligte:
    Cooper, P. A. (Autor:in) / Stroud, W. J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1972-11-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :





    Wing flutter model

    CHEN HAI / MA XIANG / HUANG GUONING et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Concerning wing-flutter

    Engineering Index Backfile | 1927