Two different wing configurations considered; for cruciform winged missile it is shown that regions of unstable controllability can exist when tail planes are rotated over 45° with respect to wings; as to annular wing configuration it is noted that, due to interference effects, favorable drag characteristics can be obtained for combination as whole.


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    Title :

    Aerodynamic aspects of design of guided missiles and rockets


    Additional title:

    Aerodynamische aspecten bij het ontwerp van geleide projectielen en raketten


    Contributors:

    Published in:

    Ingenieur ; 71 , n 39


    Publication date :

    1959


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Dutch


    Keywords :



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