Flow guide body for an aircraft

A flow guide body for an aircraft, comprising:

• a main body having an outer aerodynamic surface, the aerodynamic surface having a plurality of outlet openings;
• and
• a plurality of flow control devices, each of the plurality of flow control devices comprising:
• an inlet;
• an interaction chamber having a first end and a second end and extending from the first end to the second end along a chamber axis;
• a first outlet;
• and
• a second outlet,
• wherein the inlet is connected with the interaction chamber at the first end,
• wherein the first outlet is connected with the interaction chamber at the second end such that the first outlet projects towards a first side of the chamber axis,
• wherein the second outlet is connected with the interaction chamber at the second end such that the second outlet projects towards a second side of the chamber axis opposite the first side, and
• wherein the interaction chamber is provided with a first control inlet connected to the interaction chamber at the first side of the chamber axis,
• wherein at least one first flow control device of the plurality of flow control devices is arranged such that the first and second outlets of the first flow control device are each connected to an outlet opening in the aerodynamic surface,
• wherein the first outlet of the at least one first flow control device is provided with a first control outlet and the second outlet of the at least one first flow control device is provided with a second control outlet,
• wherein at least one second flow control device of the plurality of flow control devices is arranged such that the first or second outlet of the at least one second flow control device is connected with the inlet of the at least one first flow control device,
• wherein one of the first and second control outlets of the at least one first flow control device is connected to the first control inlet of the at least one first flow control device,
• wherein the other of the first and second control outlets of the at least one first flow control device is connected to the first or a second control inlet of the at least one second flow control device or of a third or further flow control device,
• wherein the at least one first flow control device comprises at least two first flow control devices,
• wherein the first outlet of the at least one second flow control device is connected with the inlet of one of the at least two first flow control devices,
• wherein the second outlet of the at least one second flow control device is connected with the inlet of the other of the at least two first flow control devices,
• wherein in each of the at least two first flow control devices the first control outlet is connected with the first control inlet, and
• wherein the second control outlet of that first flow control device the inlet of which is connected to the first outlet of the at least one second flow control device, is connected to the first control inlet of the at least one second flow control device.