A design and structural analysis of a CH-54B main rotor hub fabricated from composite materials was made to assess the flightworthiness of a hub consisting basically of tension straps fabricated from graphite epoxy and fiberglass. The concept is feasible but not competitive with the production titanium hub from a weight standpoint. (Author)


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    Titel :

    Design Analysis of CH-54B Main Rotor Hub Fabricated from Composite Materials


    Beteiligte:
    R. L. Faiz (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    238 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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