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

摘要

The invention relates to an aircraft wing arrangement (1) comprising a wing (2) and at least one aircraft engine attachment pylon (4) for attaching an engine suspended under the wing and comprising a forward region (8) protrudi ng forward from an leading edge (10) of the wing. According to the invention, t he forward region (8) comprises a lateral projection (12) delimiting a lateral airflow channel (14) extending towards a proximal end of the wing.