Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Computational Research of the Main Rotor Steep Descent Modes Based on the Nonlinear Blade Vortex Model


    Contributors:

    Published in:

    Publication date :

    2019




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik
    Local classification TIB:    770/7040/8000



    Computational Research of the Main Rotor Steep Descent Modes Based on the Nonlinear Blade Vortex Model

    Ignatkin, Yu. M. / Makeev, P. V. / Shaidakov, V. I. et al. | Springer Verlag | 2019


    Computational Research of the Main Rotor Hover and Vertical Descent States Based on the Nonlinear Blade Vortex Model

    Ignatkin, Yu. M. / Makeev, P. V. / Shaidakov, V. I. et al. | Springer Verlag | 2018


    Computational Research of the Main Rotor Hover and Vertical Descent States Based on the Nonlinear Blade Vortex Model

    Ignatkin, Yu. M. / Makeev, P. V. / Shaidakov, V. I. et al. | Online Contents | 2018


    MAIN ROTOR BLADE TIP VORTEX CHARACTERIZATION

    Coletta, M. / Gregorio, F. De / Visingardi, A. et al. | TIBKAT | 2020