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.


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    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






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    Walchli, L. A. / Moorhouse, D. J. / Advisory Group for Aerospace Research and Development; Flight Vehicle Integration Panel | British Library Conference Proceedings | 1997


    Forebody vortex control

    Malcolm, Gerald N. | Elsevier | 1991