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An exhaust nozzle assembly provides fluidic thrust vectoring of the primary stream to enhance aircraft maneuverability. The exhaust nozzle assembly includes a cooling air passage that supplies cooling air to a plurality of cooling holes that generate an insulating layer of air. A vector slot inject

An exhaust nozzle assembly provides fluidic thrust vectoring of the primary stream to enhance aircraft maneuverability. The exhaust nozzle assembly includes a cooling air passage that supplies cooling air to a plurality of cooling holes that generate an insulating layer of air. A vector slot injects cooling airflow into the exhaust passage normal to the primary stream. A cover plate partially blocks the vector slot to direct cooling airflow into the exhaust passage that in turn directs portions of the primary stream.

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What is claimed is: 1. An exhaust nozzle assembly for fluidic vectoring of a primary stream comprising: an exhaust passage for directing a primary stream; a duct wall defining an airflow passage for cooling air; a vector slot within said duct wall open to said exhaust passage providing a flow of co

What is claimed is: 1. An exhaust nozzle assembly for fluidic vectoring of a primary stream comprising: an exhaust passage for directing a primary stream; a duct wall defining an airflow passage for cooling air; a vector slot within said duct wall open to said exhaust passage providing a flow of cooling air from said airflow passage into said exhaust passage; wherein said vector slot is arc shaped having an apex and distal ends, said apex disposed downstream of said distal ends; and a cover movable for blocking a portion of said flow of cooling air from said airflow passage into said exhaust passage for selectively directing said primary stream. 2. The assembly as recited in claim 1, wherein said exhaust passage comprises a trailing edge and said apex is disposed closer to said trailing edge than said distal ends. 3. The assembly as recited in claim 1, wherein said slot is of a constant width. 4. The assembly as recited in claim 1, including an actuator arm attached to said cover for selectively positioning said cover over a portion of said vector slot. 5. The assembly as recited in claim 4, wherein said cover selectively directs said flow of cooling air into said exhaust passage to provide yaw vectoring. 6. The assembly as recited in claim 1, wherein the flow of cooling air through said vector slot is normal to a primary jet stream through said exhaust passage. 7. An exhaust nozzle assembly for fluidic vectoring of a primary stream comprising: an exhaust passage for directing a primary stream, wherein said exhaust passage is rectangular; a duct wall defining an airflow passage for cooling air; a vector opening within said duct wall open to said exhaust passage providing a flow of cooling air from said airflow passage into said exhaust passage; and a cover smaller than said vector opening such that some portion of the vector opening is always open for providing a flow of cooling air into exhaust passage regardless of a position of said cover, said cover movable for blocking a portion of said flow of cooling air from said airflow passage into said exhaust passage for selectively directing said primary stream. 8. An exhaust nozzle assembly for fluidic vectoring of a primary stream comprising: an exhaust passage for directing a primary stream; a duct wall defining an airflow passage for cooling air; a vector opening within said duct wall open to said exhaust passage providing a flow of cooling air from said airflow passage into said exhaust passage, wherein said vector opening comprises a plurality of vector holes disposed within an arc having an apex and distal ends; and a cover movable for blocking a portion of said flow of cooling air from said airflow passage into said exhaust passage for selectively directing said primary stream. 9. The assembly as recited in claim 8, wherein said apex is disposed downstream of said distal ends. 10. The assembly as recited in claim 8, wherein said duct wall includes a plurality of cooling holes for said cooling air, wherein said plurality of vector holes are larger than said plurality of cooling holes. 11. The assembly as recited in claim 7, wherein a width of said exhaust passage is approximately nine times a height of said exhaust passage. 12. The assembly as recited in claim 1, wherein said exhaust passage includes a top side, a bottom side and first and second sides between said top side and bottom side, wherein said vector slot is disposed within one of said top side and bottom side. 13. A fluidic vectoring assembly for an exhaust nozzle comprising: a cover plate movable within a cooling air passage for selectively blocking a portion of a vector opening, wherein the vector opening is arc shaped for communicating an arc shaped flow of cooling air to an exhaust passage, and said cover plate blocks a portion of cooling air flow into the exhaust passage to modify a direction of flow of a primary stream. 14. The assembly as recited in claim 13, including an actuator arm attached to said cover plate for moving said cover plate to different portions of said vector opening. 15. The assembly as recited in claim 13, wherein said cover plate blocks an equal area of the vector opening for all positions of the cover plate. 16. The assembly as recited in claim 13, wherein said cover selectively directs the flow of cooling air into the exhaust passage to provide fluidic vectoring of the primary stream.