Aerodynamic member, carrier wing with aerodynamic member, computer with motion drive control module, computer program, aerodynamic assembly, and method of affecting secondary turbulence

摘要

An aerodynamic element attachable to a primary wing to extend in a longitudinal direction at an angle to a spanwise direction of the primary wing. The aerodynamic element includes a downstream end having at least two flow flaps arranged next to each other and oriented in the longitudinal direction of the aerodynamic element.