AERODYNAMIC SYSTEM FOR AN AIRCRAFT
The invention relates to an aerodynamic system (1) for an aircraft (100). The aerodynamic system (1) comprises a first aerodynamic component (10) configured to be movably coupled to a primary structure (110) of the aircraft (100), a second aerodynamic component (20) which is movably coupled to the first aerodynamic component (10) and a first panel element (11) coupled to the first aerodynamic component (10), wherein the first panel element (11) at least partially covers a gap (13) between the first aerodynamic component (10) and the second aerodynamic component (20). The aerodynamic system (1) further comprises a sealing element (30) arranged between the first aerodynamic component (10) and the second aerodynamic component (20), wherein the sealing element (30) is configured to at least partially block an airflow (40) between the first aerodynamic component (10) and the second aerodynamic component (20).