The effect of wind tunnel walls on the development of flow separation in the wing-fuselage juncture area is assessed using FUN3D’s overset and wind tunnel controller capabilities. The simulation data obtained from the in-tunnel runs are compared with the free-air simulations. The simulation results are also evaluated using measurements from the Juncture Flow Experiment.


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    Titel :

    In-Tunnel Simulations of the NASA Juncture Flow Model


    Beteiligte:

    Kongress:

    AIAA SciTech Forum ; 2021 ; Nashville, TN, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    In-Tunnel Simulations of the NASA Juncture Flow Model

    Ahmad, Nashat N. / Rumsey, Christopher L. / Carlson, Jan-Renee | AIAA | 2021


    IN-TUNNEL SIMULATIONS OF THE NASA JUNCTURE FLOW MODEL

    Ahmad, Nashat N. / Rumsey, Christopher L. / Carlson, Jan-Renee | TIBKAT | 2021



    LATTICE-BOLTZMANN VERY LARGE EDDY SIMULATIONS OF THE NASA JUNCTURE FLOW MODEL

    Duda, Benjamin M. / Laskowksi, Gregory M. | TIBKAT | 2020


    Lattice-Boltzmann Very Large Eddy Simulations of the NASA Juncture Flow Model

    Duda, Benjamin M. / Laskowksi, Gregory M. | AIAA | 2020