A shock bump (10) comprising a diverging nose (20) and a converging tail. The tail has at least one plan-form con-tour line with a pair of concave opposite sides (22, 23). The shock bump provides an improved shape with relatively low drag. Furthermore, the concave shape of the tail tends to promote the development of longitudinal vortices which can reduce shock in-duced buffet at certain operating conditions.


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    Titel :

    SHOCK BUMP


    Weitere Titelangaben:

    BOSSE ANTICHOC


    Beteiligte:
    WOOD NORMAN (Autor:in)

    Erscheinungsdatum :

    2016-04-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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