Volume 3 of a three volume report tabulates aerodynamic and thrust test data on a wind tunnel model of a guided missile with canard wings. Included are tail fin force and moment coefficients.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Transonic Wind Tunnel Tests on a Missile Model with Canard Wings. Volume III


    Contributors:

    Publication date :

    1973


    Size :

    666 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English