Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Rapid, International Design and Test of a Hybrid-Powered, Blended-Wing Body Unmanned Aerial Vehicle


    Contributors:

    Conference:

    11th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference



    Publication date :

    2011-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Rapid, International Design and Test of a Hybrid-Powered, Blended-Wing Body Unmanned Aerial Vehicle

    Koster, J. / Balaban, S. / Hillery, D. et al. | British Library Conference Proceedings | 2011


    BLENDED WING BODY TAILSITTER UNMANNED AERIAL VEHICLE (UAV)

    PUSHP NAMAN | European Patent Office | 2024

    Free access

    WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLE

    Mariani, R. / Suewatanakul, S. / Ghika, S. et al. | British Library Conference Proceedings | 2022


    Conceptual Design of a Blended-Wing-Body Tilt-Arm Hybrid Unmanned Aerial Vehicle

    Abnous, Rosa / Zeng, Chen / Chowdhury, Souma et al. | AIAA | 2017


    Unmanned aerial vehicle wing limiting mechanism, unmanned aerial vehicle wing and unmanned aerial vehicle

    ZHANG KE / ZHANG XIAOPAN / ZHANG YING et al. | European Patent Office | 2023

    Free access