Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Effect of Rotation Kinematics and Angle of Attack on Flapping Flight


    Contributors:

    Published in:

    AIAA Journal ; 47 , 11 ; 2505-2519


    Publication date :

    2009-11-01


    Size :

    15 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





    Quasi-hovering Flight of a Flapping MAV with Large Angle of Attack

    Kawamura, Y. / Souda, S. / Ellington, C.P. et al. | British Library Conference Proceedings | 2006


    A COUPLED KINEMATICS AND ENERGETICS MODEL FOR FLAPPING FLIGHT

    Salehipour, H. / Willis, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010


    A Coupled Kinematics and Energetics Model for Flapping Flight

    Salehipour, Hesam / Willis, David | AIAA | 2010


    Flapping-rotating wing with attack angle control device

    WU JIANGHAO / ZHOU CHAO / ZHANG YANLAI | European Patent Office | 2015

    Free access