An experiment was conducted to examine the vortex trapping concept on a 60 deg sweep delta wing at low angles of attack. Using tapered leading edge fences, stable vortices have been successfully trapped. The resulting increase in lift coefficient can be as high as 0.4, which amounts to a 6.5 deg shift in the lift coefficient curve of the delta wing. The corresponding increase in drag coefficient, however, is also significant.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Vortex trapping on a 60 degree delta wing


    Beteiligte:
    Buchholz, Mark D. (Autor:in) / Tso, Jin (Autor:in)

    Kongress:

    AIAA Applied Aerodynamics Conference ; 1992 ; Palo Alto, CA, United States


    Erscheinungsdatum :

    1992-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Vortex trapping on a 60 degree delta wing

    BUCHHOLZ, MARK / TSO, JIN | AIAA | 1992


    Wing loading on a 60 degree delta wing with vortex flaps

    Marchman, J. F., III / Donatelli, D. A. / Terry, J. E. | NTRS | 1983


    Wing loading on a 60 degree delta wing with vortex flaps

    MARCHMAN, III, J. / DONATELLI, D. / TERRY, J. | AIAA | 1983



    Experimental Studies of a 70-Degree Delta Wing with Vortex Flaps

    Kenichi Rinoie / Toshimi Fujita / Akihito Iwasaki et al. | AIAA | 1997