This report presents a detailed description of the flightworthy graphite fiber reinforced composite aircraft primary structural assemblies program. The following tasks have been completed: Intermediate and final demonstration item design; fabrication procedures development; hardware fabrication; demonstration item testing; specification development; and cost effectiveness evaluation. Demonstration items selected were the F-5A supersonic fighter main landing gear strut door, speed brake, wing leading edge flap, wing trailing edge flap, horizontal stabilizer, and vertical stabilizer main spar. (P.S.-PL)


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    Title :

    Flightworthy Graphite Fiber Reinforced Composite Aircraft Primary Structural Assemblies. Volume II. Tasks 6 through 12


    Contributors:
    R. D. Hayes (author)

    Publication date :

    1972


    Size :

    450 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English