Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Investigation of separation mechanism for airfoil leading edge flow at low Reynolds number


    Contributors:
    Jian, Y. (author) / Zhengping, Z. (author) / Lipeng, L. (author) / Lin, Y. (author)


    Publication date :

    2004-01-01


    Size :

    5 pages



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Unknown


    Classification :

    DDC:    629.4




    Reynolds Number Effect of Leading Edge Tubercles on Airfoil Aerodynamics

    Peristy, Luke H. / Perez, Ruben E. / Asghar, Asad et al. | AIAA | 2016