AIRCRAFT ENGINE WITH STRUT

An aircraft engine includes an air inlet duct and at least one strut having a leading edge and a trailing edge (31B). The at least one strut (30) extends across at least part of the air inlet duct and has a strut passage. The trailing edge (31B) has one or more edge contours (39), each defining a contour edge wall (39W) recessed from a baseline surface (31 BS) of the trailing edge (31B). The one or more edge contours (39) have a recessed tap (38) in fluid communication with the strut passage.