| 摘要 |
<p>The aircraft (1) has a pair of wings (6, 8) arranged at a side of a fuselage (2). A fairing (12) comprises a fairing surface connected to a lower surface (42) of each wing and extending longitudinally in a direction of a longitudinal axis of the fuselage, where the aircraft is made asymmetry or lateral dissymmetry such that center of gravity of the aircraft is not situated in a symmetry plane. The fairing surface has a local geometric deformation adapted to produce a corrective rolling moment (34) to compensate for undesirable rolling moment (27) produced by the lateral dissymmetry.</p> |
