An aerodynamic arrangement and method for providing a required air pressure coefficient at an area of location of an air port of an internal cooling system of a flying platform is described. The air port is selected from an air inlet port and an air outlet port, and arranged at a desired area in an external surface of the flying platform. The aerodynamic arrangement includes at least one airfoil-shaped body arranged on the external surface at the area of the air port for providing a negative pressure coefficient at the corresponding desired area on one side of the airfoil-shaped body and a positive pressure coefficient at the corresponding desired area on the other side of the airfoil-shaped body, when the airfoil-shaped body is oriented at a suitable angle of attack to an oncoming air flow.
AIRBORNE AERODYNAMIC ARRANGEMENT
2020-09-03
Patent
Electronic Resource
English