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    Title :

    Numerical Aerodynamic Investigations on Missile Yawing Control Using Nose-Mounted Flow Effectors



    Published in:

    Publication date :

    2008



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Unknown



    Classification :

    Local classification TIB:    770/7040
    BKL:    55.60 Raumfahrttechnik




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