Structural features and approach employed in design of high-performance light aircraft stressed to 8 g limit loads; analytical design exercise shows feasibility of constructing primary airframe from fibrous composite materials; results of minimum weight analyses of fluted core and honeycomb core sandwich panels and their use in selection of final sandwich geometry; curves showing variation in elastic properties with changes in fiber orientation angle for typical basic laminate patterns employed in airframe components.


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    Titel :

    Design of aircraft utilizing fiberglass reinforced plastic primary structure


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Noyes, J.V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    FIBERGLASS REINFORCED PLASTIC TRUCK BODIES

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    Fiberglass reinforced plastic truck bodies

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    MOORING BUOY MADE OF FIBERGLASS REINFORCED PLASTIC

    YUEN ALEX | Europäisches Patentamt | 2024

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