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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    Titel :

    Aerodynamic aspects of design of guided missiles and rockets


    Weitere Titelangaben:

    Aerodynamische aspecten bij het ontwerp van geleide projectielen en raketten


    Beteiligte:
    Erdmann, S.F. (Autor:in)

    Erschienen in:

    Ingenieur ; 71 , n 39


    Erscheinungsdatum :

    1959


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Niederländisch


    Schlagwörter :



    The handbook of rockets and guided missiles

    Bowman, Norman J. | GWLB - Gottfried Wilhelm Leibniz Bibliothek | 1957


    Rockets and missiles

    Nicholas, John | TIBKAT | 1989


    Guided missiles -- Some devices for controlling long range rockets

    White, G. | Engineering Index Backfile | 1947


    Guided Rockets and Missiles, Class Air-to-Air - Poland

    T. Burakowski / A. Sala | NTIS | 1960