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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    Title :

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


    Contributors:
    J. Ross (author) / M. Denison (author) / R. Childs (author) / J. Garcia (author) / P. Stremel (author) / V. Hawke (author) / H. Spooner (author) / M. A. Reed (author) / B. Kleb (author) / A. N. Watkins (author)

    Publication date :

    2021


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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    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

    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