The design and operation of very large, long-range, subsonic cargo aircraft are considered. A design concept which distributes the payload along the wingspan to counterbalance the aerodynamic loads, with a resultant decrease in the in-flight wing bending moments and shear forces, is described. The decreased loading of the wing structure, coupled with the very thick wing housing the cargo, results in a relatively low overall structural weight in comparison to that of conventional aircraft.


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    Titel :

    Design of a Large Span-Distributed Load Flying-Wing Cargo Airplane


    Beteiligte:
    L. S. Jernell (Autor:in) / C. B. Quartero (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    99 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Design of a Large Span-Distributed Load Flying-Wing Cargo Airplane

    Jernell, L. S. / Quartero, C. B. | NTRS | 1977




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