An analytical study of the mutual interaction between a wake vortex and an encountering airplane has been conducted. The interaction was calculated on the basis of conservation of angular momentum of the wake vortex and the encountering airplane in the roll axis. For the nominal conditions assumed in the study, the interaction reduced the roll response in the lust second by 20 percent compared to the classical method of calculating the response. However, depending on the conditions assumed, the reduction varied from 0 to 30 percent which could be highly significant in determining separation standards for airplanes. Controlled experiments are needed to determine the exact amount of interaction.


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    Titel :

    A study of the interaction between a wake vortex and an encountering airplane


    Beteiligte:
    Stewart, E. C. (Autor:in)

    Kongress:

    AIAA, Atmospheric Flight Mechanics Conference ; 1993 ; Monterey, CA, United States


    Erscheinungsdatum :

    1993-08-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    A Study of the Interaction between a Wake Vortex and an Encountering Airplane

    Stewart, E. / AIAA | British Library Conference Proceedings | 1993


    A Dynamic Analysis of Aeroplanes Encountering Vortex Wake Turbulence

    R. C. H. Parkinson / D. W. Kelly | NTIS | 1973


    Flight-test experience of a helicopter encountering an airplane trailing vortex

    Dunham, R. E., Jr. / Holbrook, G. T. / Campbell, R. L. et al. | NTRS | 1976


    Theory of an airplane encountering gusts II

    Wilson, Edwin Bidwell | NTRS | 1918