An air vehicle (100, 102) having a bilaterally asymmetric configuration may include a body (104) having a longitudinal axis (106). The air vehicle (100, 102) may further include longitudinally offset engine nacelles (234, 236), asymmetrically lengthened engine nacelles (232), and/or longitudinally offset protruding aerodynamic surfaces (190). (Fig. 1)


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    Title :

    System and method for minimizing wave drag through bilaterally asymmetric design


    Additional title:

    System und Verfahren zur Minimierung von Wellenwiderstand durch bilateral asymmetrisches Design
    Système et procédé permettant de réduire la traînée d'onde par conception asymétrique de manière bilatérale


    Contributors:

    Publication date :

    2017-01-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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