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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    Title :

    Aerodynamic Loads on Aircraft Encountering Vortex Wakes of Other Aircraft


    Additional title:

    Foundations Engineering Mechanics


    Contributors:


    Publication date :

    2009-06-13


    Size :

    20 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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    Aircraft vortex wakes

    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