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)
System and method for minimizing wave drag through bilaterally asymmetric design
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
18.01.2017
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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