From the literature, theoretical analyses and subscale windtunnel aerodynamic investigations of canard aircraft configurations indicate benefits which are enhanced by close-coupling the canard to the wing. To properly evaluate the advantages and to investigate some solutions to the problems associated with the close-coupled canard, a full-scale aircraft development was initiated. A dual purpose of this development was to create a proof-of-concept vehicle designed to satisfy a general aviation requirement, and demonstrate a subsonic, close-coupled canard technology. This paper describes the development together with the aerodynamic considerations of the design. Ultimately, flight-test data are to be used in establishing correlations with windtunnel model data and analytical methodology.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    A close-coupled canard, technology demonstration aircraft for general aviation applications


    Weitere Titelangaben:

    Mit Tragflaechen gekoppeltes kopfgesteuertes Flugzeug: Demonstration der Technik fuer den allgemeinen Luftverkehr


    Beteiligte:
    Martin, J.D. (Autor:in) / Foster, N.R. (Autor:in)

    Erschienen in:

    SAE-Papers ; Oct ; 1-9


    Erscheinungsdatum :

    1987


    Format / Umfang :

    9 Seiten, 13 Bilder, 20 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    A Close-Coupled Canard, Technology Demonstration Aircraft for General Aviation Applications

    Martin, Joe. D. / Foster, Ned R. | SAE Technical Papers | 1987


    Exploiting the close-coupled canard

    MARTIN, J. / FOSTER, N. | AIAA | 1987


    Exploiting the close-coupled canard

    Martin, J.D. / Foster, N.R. | Tema Archiv | 1987