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
System and method for minimizing wave drag through bilaterally asymmetric design
16.02.2017
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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