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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    F-8 oblique wing structural feasibility study


    Beteiligte:
    Koltko, E. (Autor:in) / Katz, A. (Autor:in) / Bell, M. A. (Autor:in) / Smith, W. D. (Autor:in) / Lauridia, R. (Autor:in) / Overstreet, C. T. (Autor:in) / Klapprott, C. (Autor:in) / Orr, T. F. (Autor:in) / Jobe, C. L. (Autor:in) / Wyatt, F. G. (Autor:in)

    Erscheinungsdatum :

    1975-11-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    F-8 Oblique Wing Structural Feasibility Study

    E. Koltko / A. Katz / M. A. Bell et al. | NTIS | 1975


    Oblique Wing Aerodynamics

    McDaniel, Melissa / Wilks, Brett | AIAA | 2004


    Oblique Wing Aerodynamics

    M. A. McDaniel / B. L. Wilks | NTIS | 2004


    Oblique Wing Aircraft

    Torenbeek, Egbert | Wiley | 2020


    Oblique-wing supersonic aircraft

    Jones, R. T. | NTRS | 1976