It has been shown by a new static airflow visualization method that a drogue device properly positioned downstream of the wing tip causes vortex breakdown. This same result has been obtained by mounting a jet engine simulator at the wing tip and directing the high-energy jet blast downstream into the vortex. These configurations, among others, are now under intensive investigation in the new Langley Vortex Research Facility. In this facility a balance mounted vortex generating model is propelled along the 1800-foot track while a second model trailed at 160 feet (scale distance of 1 mile) measures the far-field rolling moment induced by the vortex of the generating model.


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    Titel :

    Lift-induced wing-tip vortex attenuation


    Beteiligte:

    Kongress:

    Aerospace Sciences Meeting ; 1974 ; Washington, DC


    Erscheinungsdatum :

    1974-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Lift-induced wing-tip vortex attenuation

    PATTERSON, JR., J. | AIAA | 1974


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