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    Titel :

    Detached Eddy Simulation of Flow over NACA0012 Airfoil at High Angle of Attack with Spectral Difference Method (AIAA 2014-0425)



    Kongress:

    52nd, Aerospace sciences meeting; held at the AIAA SciTech Forum 2014 ; 2014 ; National Harbor, MD



    Erscheinungsdatum :

    2014-01-01


    Format / Umfang :

    15 pages


    Anmerkungen:

    Includes bibliographical references and author index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    AIAA 2001-0425 LARGE EDDY SIMULATION OF THE FLOW AROUND AN AIRFOIL

    Dahlstrom, S. / Davidson, L. / AIAA | British Library Conference Proceedings | 2001


    DELAYED DETACHED EDDY SIMULATION OF A STALL FLOW OVER NACA0012 AIRFOIL USING HIGH ORDER SCHEMES

    Im, H. / Zha, G. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011



    Detached-Eddy Simulation of a Co-Flow Jet Airfoil at High Angle of Attack

    Wang, B. / Zha, G. / American Institute of Aeronautics and Asronautics | British Library Conference Proceedings | 2009