A prior study conducted for the Naval Air Systems Command for application of advanced composites in the XFV-12A aircraft indicated the wing torque box to be the component of airframe structure having the greatest potential for significant weight savings through composite material application. A Phase II design/development program was undertaken to develop detail design concepts for a XFV-12A composite wing box and fabricate a representative section of this wing box for development test and evaluation to provide a base for subsequent Phase III full scale verification testing.


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    Titel :

    Evaluation of Composite Wing for XFV-12A Airplane


    Beteiligte:
    D. N. Ulry (Autor:in) / R. W. Gehring (Autor:in) / K. I. Clayton (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    326 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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