A deployable system is introduced for assisting flight control under certain flight conditions, such as at high angles of attack, whereby two inflatable membranes are located on the forebody portion of an aircraft on opposite sides thereof. The members form control surfaces for effecting lateral control forces if one is inflated and longitudinal control forces if both are inflated.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic surface distension system for high angle of attack forebody vortex control


    Beteiligte:
    Zell, Peter T. (Autor:in)

    Erscheinungsdatum :

    1994-07-05


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch






    The Impact of Forebody Geometries at High-Angle-of-Attack with Forebody Tangential Blowing

    Chow, J. / Pedreiro, N. / Rock, S. et al. | British Library Conference Proceedings | 1998


    Forebody vortex management for yaw control at high angles of attack

    Rao, Dhanvada M. / Murri, Daniel G. / Moskovitz, Cary | NTRS | 1987


    Forebody vortex management for yaw control at high angles of attack

    RAO, DHANVADA M. / MURRI, DANIEL G. / MOSKOVITZ,CARY | AIAA | 1987