The investigation deals with the dynamic behavior of an airplane encountering aircraft wake turbulence. A digital computer simulation was developed to study the response of an aircraft flying into a trailing vortex wake. The simulation includes the complete six degree of freedom equations of motion, a description of the vortex velocity field, unsteady aerodynamics, and pilot control input. The parameters included the penetration angle, separation distance, aircraft size, and pilot control input. Predicted vortex induced motions are presented for general aviation, business, and light jet transport type aircraft. (Modified author abstract)


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    Titel :

    The Response of Aircraft Encountering Aircraft Wake Turbulence


    Beteiligte:
    R. C. Nelson (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    141 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch