AIRCRAFT AND METHOD OF COUNTERING AERODYNAMIC EFFECTS OF PROPELLER WAKE�

摘要

ABSTRACT OF THE DISCLOSURE AIRCRAFT AND METHOD OF COUNTERING AERODYNAMIC EFFECTS OF PROPELLER WAKE Aircraft having a fuselage having a centerline, a wing extending from the fuselage and having a leading edge and a trailing edge, an engine mounted to the wing and having a rotating output shaft, a propeller operably coupled to the output shaft and generating a rotating flow field to define a propeller wake when the propeller is rotated by the rotating output shaft and a method of countering the aerodynamic effects of propeller wake acting on a wing.