Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    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 Forum and Exposition ; 2020 ; Orlando, Fla.



    Publication date :

    2020


    Type of media :

    Conference paper


    Type of material :

    Print


    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