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    Title :

    Numerical study of UAS-S4 Éhecatl aerodynamic performance improvement obtained with the use of a morphing wing approach


    Contributors:

    Conference:

    33rd AIAA Applied Aerodynamics Conference



    Publication date :

    2015-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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