Underwing compression vortex-attenuation device designed to provide method for attenuating lift-induced vortex generated by wings of airplane. Includes compression panel attached to lower surface of wing, facing perpendicular to streamwise airflow. Concept effective on all types of aircraft. Causes increase in wing lift rather than reduction when deployed. Device of interest to aircraft designers and enhances air safety in general.


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    Titel :

    Underwing Compression Vortex-Attenuation Device


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.11.1994



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :





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