Aerodynamic system for an aircraft

An aerodynamic system for an aircraft, comprising:

• a first aerodynamic component configured to be movably coupled to a primary structure of the aircraft;
• a second aerodynamic component which is movably coupled to the first aerodynamic component;
• a first panel element coupled to the first aerodynamic component, wherein the first panel element at least partially covers a gap between the first aerodynamic component and the second aerodynamic component;
• a sealing element arranged between the first aerodynamic component and the second aerodynamic component, wherein the sealing element is configured to at least partially block an airflow between the first aerodynamic component and the second aerodynamic component,
• wherein the sealing element is arranged between a nose section of the second aerodynamic component and a trailing edge section of the first aerodynamic component;
• wherein the second aerodynamic component comprises a recess at the nose section of the second aerodynamic component;
• wherein the aerodynamic system further comprises a nose support element which is received within the recess at the nose section of the second aerodynamic component;
• and
• wherein the sealing element is arranged between the nose support element of the second aerodynamic component and the trailing edge section of the first aerodynamic component.