Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Effects of Asymmetric Blade-Pitching Kinematics on Forward-Flight Performance of a Micro-Air-Vehicle-Scale Cycloidal-Rotor



    Published in:

    Publication date :

    2016




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

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




    Symmetric Versus Asymmetric Pitching of a Cycloidal Rotor Blade at Ultra-Low Reynolds Numbers

    Walther, Carolyn M. / Saemi, Farid / Benedict, Moble et al. | AIAA | 2019


    Effect of Flow Curvature on Forward Flight Performance of a Micro-Air-Vehicle-Scale Cycloidal-Rotor

    Benedict, Moble / Jarugumilli, Tejaswi / Lakshminarayan, Vinod et al. | AIAA | 2014



    Effect of Rotor Geometry and Blade Kinematics on Cycloidal Rotor Hover Performance

    Benedict, Moble / Jarugumilli, Tejaswi / Chopra, Inderjit | AIAA | 2013