The feasibility of fitting a rotating oblique wing on an F-8 aircraft to produce a full scale manned prototype capable of operating in the transonic and supersonic speed range was investigated. The strength, aeroelasticity, and fatigue life of such a prototype are analyzed. Concepts are developed for a new wing, a pivot, a skewing mechanism, control systems that operate through the pivot, and a wing support assembly that attaches in the F-8 wing cavity. The modification of the two-place NTF-8A aircraft to the oblique wing configuration is discussed.


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    Titel :

    F-8 Oblique Wing Structural Feasibility Study


    Beteiligte:
    E. Koltko (Autor:in) / A. Katz (Autor:in) / M. A. Bell (Autor:in) / W. D. Smith (Autor:in) / R. Lauridia (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    151 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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