The medium around the aircraft in hand is taken to be an ideal incompressible fluid, the aircraft’s surfaces are assumed impermeable. The flow is potential everywhere outside the aircraft and its vortex wake. The vortex wake represents a thin vortex sheet, i.e., a surface with a jump of the tangential component of the velocity field. The flow separation lines are taken to be the sharp edges of the aircraft’s surface.


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    Titel :

    Aerodynamic Loads on Aircraft Encountering Vortex Wakes of Other Aircraft


    Weitere Titelangaben:

    Foundations Engineering Mechanics


    Beteiligte:


    Erscheinungsdatum :

    2009-06-13


    Format / Umfang :

    20 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    REAL TIME MATHEMATICAL MODELING OF THE AERODYNAMIC CHARACTERISTICS OF AN AIRCRAFT ENCOUNTERING VORTEX WAKES

    Gaifullin, A. / Kornyakov, A. / Sviridenko, Y. et al. | British Library Conference Proceedings | 2010


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    Boswinkle, R. W., Jr. | NTRS | 1970


    Vortex wakes of conventional aircraft

    Donaldson, Coleman / Bilanin, Alan J. | TIBKAT | 1975


    Vortex Wakes of Conventional Aircraft

    C. P. Donaldson / A. J. Bilanin | NTIS | 1975


    Vortex Wakes of large aircraft

    Donaldson, C. D. ;Bilanin, A. J. | TIBKAT | 1974