The materials and advanced producibility methods that offer potential structural mass savings in the design of the primary structure for a supersonic cruise aircraft are identified and reported. A summary of the materials and fabrication techniques selected for this analytical effort is presented. Both metallic and composite material systems were selected for application to a near-term start-of-design technology aircraft. Selective reinforcement of the basic metallic structure was considered as the appropriate level of composite application for the near-term design.


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    Title :

    Arrow-wing supersonic cruise aircraft structural design concepts evaluation. Volume 2: Sections 7 through 11


    Contributors:

    Publication date :

    1975-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English