Wind-tunnel tests were made to investigate the control effectiveness of wing trailing-edge flap-type aerodynamic controls for a supercritical wing. The tests determined the effects of spanwise flap control location, two different wing transition grit location patterns, magnitude of angular control deflection, control hinge moments and control hinge gap seals. Results show that the inboard flap position deflections caused interference rearward at the vertical tail, and that all flap positions for deflections in one direction only caused interference at the horizontal tail at a higher than design Mach number. Changes in wing transition grit pattern caused significant changes to static longitudinal characteristics and longitudinal control effectiveness.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Wing flap-type control effectiveness and effects of control hinge gap seals for a supercritical wing


    Beteiligte:
    Anglin, E. L. (Autor:in) / Byrdsong, T. A. (Autor:in)

    Kongress:

    Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference ; 1982 ; St. Louis, MO


    Erscheinungsdatum :

    1982-06-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    WING FLAP DEFLECTION CONTROL REMOVAL

    JAN A KORDEL / JACOB DANIEL VIRNIG / MICHAEL ALBERT BALZER et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    WING FLAP DEFLECTION CONTROL REMOVAL

    KORDEL JAN A / VIRNIG JACOB DANIEL / BALZER MICHAEL ALBERT et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    WING FLAP DEFLECTION CONTROL REMOVAL

    KORDEL JAN A / VIRNIG JACOB DANIEL / BALZER MICHAEL ALBERT et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    AIRPLANE WING FLAP CONTROL DEVICE

    BOBROVICH VLADIMIR ALEKSANDROVICH / KORNEEV ALEKSANDR NIKOLAEVICH / PIATIKOP ALEKSEI VIKTOROVICH | Europäisches Patentamt | 2022

    Freier Zugriff