| 摘要 |
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 |
