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    Title :

    The study of the effect of the cavity on the flow over NACA 0012 and Selig 7003 aerofoil at Low Reynolds number using Vortex Shading Method


    Contributors:

    Conference:

    AIAA Scitech 2020 Forum



    Publication date :

    2020-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English







    Aeroacoustic Study on a NACA 0012 Aerofoil

    Swales, C. / Lowson, M. V. / AIAA | British Library Conference Proceedings | 1997


    Aero-acoustic study on a NACA 0012 aerofoil

    Swales, C. / Lowson, M. | AIAA | 1997