Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Analysis of aerodynamic characteristics using the vortex lattice method on twin tail boom unmanned aircraft


    Contributors:

    Conference:

    International Seminar of Aerospace Science and Technology ; 7. ; 2019 ; Jakarta



    Publication date :

    2020



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Classification :

    BKL:    55.50 Luftfahrzeugtechnik



    Static stability analysis on twin tail boom UAV using numerical method

    Septiyana, Angga / Ramadiansyah, M. Lutfi / Jayanti, Eries Bagita et al. | TIBKAT | 2021


    On the Design and Aeroelastic Stability Analysis of Twin Wing-Tail Boom Configuration Unmanned Air Vehicle

    Ozozturk, S. / Kayran, A. / Alemdaroglu, N. et al. | British Library Conference Proceedings | 2011


    Deep-stall aerodynamic characteristics of t-tail aircraft

    Ray, E. J. / Taylor, R. T. | NTRS | 1965


    Double-tail-boom tail folding mechanism of unmanned aerial vehicle

    YAN ZIHUI / FANG LIBO | European Patent Office | 2022

    Free access

    On the Design and Aeroelastic Stability Analysis of Twin Wing-Tail Boom Configuration Unmanned Air Vehicle

    Özöztürk, Sedat / Kayran, Altan / Alemdaroglu, Nafiz et al. | AIAA | 2011