Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

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


    Beteiligte:
    Koster, J. (Autor:in) / Balaban, S. (Autor:in) / Hillery, D. (Autor:in) / Serani, E. (Autor:in) / Velazco, A. (Autor:in) / Humbargar, C. (Autor:in) / Goodman, C. (Autor:in) / Brewer, A. (Autor:in) / Johnson, M. (Autor:in) / Kosyan, M. (Autor:in)

    Kongress:

    Conference; 11th, Aviation technology, integration and operations; ATIO conference, including the AIAA balloon systems conference and 19th AIAA lighter-than-air technology conference 2011 ; 2011 ; Virginia Beach, VA



    Erscheinungsdatum :

    01.01.2011


    Format / Umfang :

    7 pages


    Anmerkungen:

    Includes bibliographical references and author index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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

    Koster, Jean / Munz, Claus-dieter / Kraemer, Ewald et al. | AIAA | 2011


    BLENDED WING BODY TAILSITTER UNMANNED AERIAL VEHICLE (UAV)

    PUSHP NAMAN | Europäisches Patentamt | 2024

    Freier Zugriff

    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. | Europäisches Patentamt | 2023

    Freier Zugriff