Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Flight Investigation from Mach Number 0.8 to 2.0 to Determine Some Effects of Wing-to-tail Distance on the Longitudinal Stability and Control Characteristics of a 60 Degree Delta-wing-canard Missile


    Contributors:

    Publication date :

    1952-06-20


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English