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    Title :

    Effect of large deflection of a canard control and deflections of a wing-tip control on the static-stability and induced-roll characteristics of a cruciform canard missile at a Mach number of 2.01


    Contributors:

    Publication date :

    1953-12-14


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English