Design concepts are presented and evaluated for the application of fiber reinforced composite materials to fuselage structures. The concepts are evaluated on the basis of cost-effectiveness and performance when specifically applied to the aft fuselage of the Army AH-1G helicopter. Comparisons to the existing metal structure show that several of the new concepts provide significant advantages in initial acquisition cost, life-cycle cost, weight, safety, reliability, and maintainability. (Author)


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    Titel :

    Investigation of Advanced Structural Concepts for Fuselage


    Beteiligte:
    R. J. Mayerjak (Autor:in) / W. A. Smyth (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    148 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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