AIRCRAFT WING ARRANGEMENT COMPRISING AN ENGINE ATTACHMENT STRUT DEFINING IN THE FRONT ZONE A LATERAL AIR FLOW CHANNEL

摘要

The invention relates to an aircraft wing arrangement comprising a wing and at least one strut for attaching the aircraft engine suspended under the wing and comprising a front zone situated projecting towards the front with respect to a leading edge of the wing. According to the invention, the front zone comprises a lateral projection delimiting a lateral airflow channel while being projected towards a proximal end of the wing. One technical problem addressed by the present invention relates to aerodynamic continuity and efficiency for wings having an aircraft engine closely suspended under the wing.