| 摘要 |
<p>The nacelle has panels (50, 50') placed end to end along longitudinal direction, where the panels respectively include aerodynamic surfaces (52, 52') in contact with an air stream and edges (54, 54') in contact with each other. One of the panels comprises a partition (58) at the edge. The partition projects relative to the edge that extends in the direction of the edge of another panel, in a manner that is secant to one of the aerodynamic surfaces and in a plane that is in the longitudinal direction so as to limit circulation of air between the edges of the panels.</p> |
