The artificial viscosity method of Kuwahara and Takami (1973) is used to calculate the roll-up of trailing vortices behind a number of practical aerodynamic configurations. Where possible, the results are compared for core location with available experimental data.


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    Title :

    Roll-up of aircraft trailing vortices using artificial viscosity


    Contributors:
    Bloom, A. M. (author) / Jen, H. (author)

    Published in:

    Publication date :

    1974-11-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Roll-up of aircraft trailing vortices using artificial viscosity

    BLOOM, A. M. / George Washington University / Washington et al. | AIAA | 1974


    Merging of Aircraft Trailing Vortices

    Steven A. Brandt / James D. Iversen | AIAA | 1977


    Merging of aircraft trailing vortices

    BRANDT, S. / IVERSEN, J. | AIAA | 1977


    Analytical studies of aircraft trailing vortices

    KUHN, G. / NIELSEN, J. | AIAA | 1972


    Numerical Simulation of Aircraft Trailing Vortices

    F. H. Proctor / G. F. Switzer | NTIS | 2000