Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Roll divergence of a Canard-controlled missile with freely spinning tail


    Contributors:
    HANIN, M. (author)

    Conference:

    10th Atmospheric Flight Mechanics Conference ; 1983 ; Gatlinburg , TN , U.S.A.



    Publication date :

    1983-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English







    Aerodynamic Characteristics of a Canard-Controlled Missile with a Free-Spinning Tail

    Auman, L. M. / Kreeger, R. E. / AIAA | British Library Conference Proceedings | 1998


    AIAA-2003-3670 Cartesian-Grid Simulations of a Canard-Controlled Missile with a Spinning Tail

    Murman, S. / Aftosmis, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003