SYSTEM AND METHOD FOR MINIMIZING WAVE DRAG THROUGH BILATERALLY ASYMMETRIC DESIGN An air vehicle (100) having a bilaterally asymmetric configuration may include a body (104) having a longitudinal axis (106). The air vehicle (100) may further include longitudinally offset engine nacelles (232), asymmetrically lengthened engine nacelles (232), and/or longitudinally offset protruding aerodynamic surfaces (190). 04 CN Co CN CN C\I 'C 0 00c CD Co C,4 CN 0 CN r- C%4C) CNC0 C*4 o 00


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    Title :

    System and method for minimizing wave drag through bilaterally asymmetric design


    Contributors:

    Publication date :

    2017-02-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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