AIR INLET STRUT FOR AIRCRAFT ENGINE

An aircraft engine comprises an air inlet duct (21) extending from an inlet (25) through which air is configured to enter the aircraft engine, to an outlet within the aircraft engine. At least one strut (30) has a leading edge (31A) and a trailing edge (31B) and extends across at least part of the air inlet duct (21). The at least one strut (30) has a strut passage (33) and a plurality of static pressure measurement taps (38) spaced apart on the trailing edge (31B) and in fluid communication with the strut passage (33).