This is the set of slides describing the CFD and wind-tunnel test studying the control surfaces of the CobraMRV concept for entry, descent, and landing on Mars. Difference between the CFD and wind-tunnel results are highlighted with the intent of showing whether CFD can replace wind-tunnel testing in the high supersonic flight regime.


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    Titel :

    Evaluation of CFD for Simulation of High-Supersonic Control Surface Effectiveness


    Beteiligte:
    Jim Ross (Autor:in) / Marie Denison (Autor:in) / Robert Childs (Autor:in) / Joseph Garcia (Autor:in) / Paul Stremel (Autor:in) / Veronica Hawke (Autor:in) / Hannah Spooner (Autor:in) / M. Alec Reed (Autor:in) / Bil Kleb (Autor:in) / A. Neal Watkins (Autor:in)

    Kongress:

    AIAA Aviation Forum ; 2021 ; Virtual, US


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Evaluation of CFD for Simulation of High-Supersonic Control-Surface Effectiveness

    Ross, James C. / Denison, Marie / Childs, Robert et al. | AIAA | 2021



    Evaluation of CFD for Simulation of High-Supersonic Control-Surface Effectiveness

    James C. Ross / Marie F. Denison / Robert E. Childs et al. | NTRS


    EVALUATION OF CFD FOR SIMULATION OF HIGH-SUPERSONIC CONTROL-SURFACE EFFECTIVENESS

    Ross, James C. / Denison, Marie / Childs, Robert et al. | TIBKAT | 2021


    Evaluation of CFD for Simulation of High-Supersonic Control-Surface Effectiveness

    James C Ross / Marie F Denison / Robert E Childs et al. | NTRS