A brief overview of the highlights of NASA's wake vortex minimization program is presented. The significant results of this program are summarized as follows: (1) it is technically feasible to reduce significantly the rolling upset created on a trailing aircraft; (2) the basic principles or methods by which reduction in the vortex strength can be achieved have been identified; and (3) an analytical capability for investigating aircraft vortex wakes has been developed.


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    Titel :

    Wake vortex technology


    Beteiligte:
    Dunham, R. E., Jr. (Autor:in) / Barber, M. R. (Autor:in) / Croom, D. R. (Autor:in)


    Erscheinungsdatum :

    1978-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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