Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Determination of Rotary Wing MAV Stability Derivatives in Hover Using a Forced Oscillation Test Stand



    Conference:

    Annual forum; 61st, American Helicopter Society ; 2005 ; Grapevine, TX



    Publication date :

    2005-01-01


    Size :

    9 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    Rotary-wing, hover-capable aircraft and methods

    BENEDICT MOBLE / DENTON HUNTER J / KANG HAO et al. | European Patent Office | 2024

    Free access

    ROTARY-WING, HOVER-CAPABLE AIRCRAFT AND METHODS

    BENEDICT MOBLE / DENTON HUNTER / KANG HAO et al. | European Patent Office | 2021

    Free access

    ROTARY-WING, HOVER-CAPABLE AIRCRAFT AND METHODS

    BENEDICT MOBLE / DENTON HUNTER J / KANG HAO et al. | European Patent Office | 2022

    Free access

    Determination of dynamic stability derivatives using forced oscillation technique

    Alemdaroglu, N. / Iyigun, I. / Altun, M. et al. | AIAA | 2002


    ROTOR HOVER FIGURE OF MERIT FOR ROTARY WING AIRCRAFT

    EADIE WILLIAM J / EGOLF THOMAS ALAN / MOFFITT ROBERT C | European Patent Office | 2017

    Free access