US Patent 9908617 Active flow control for transonic flight
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Patent abstract
An air vehicle includes an airfoil designed for transonic flight. The airfoil has a region of supersonic flow during transonic flight. A surface of the airfoil has upstream and downstream orifices at or within the region. The air vehicle further includes an active flow control system for controlling air vehicle motion during transonic flight by controlling flow through the orifices to alter strength and location of a shock wave in the region. The system creates an aerodynamic imbalance to move the shock wave.
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Patent Inventor Names
Ahmed A. Hassan0
Casey L. Madsen0
Garrett M Billman0
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US Patent 09908617 Active flow control for transonic flight US Patent 9908617 Active flow control for transonic flight
Infobox
Patent Number
099086170
Patent Number
99086170
Edits on 2 Apr, 2023
Golden AI
Infobox
Is a
Patent Jurisdiction
Patent Number
099086170
Date of Patent
March 6, 2018
0Patent Application Number
131140060
Date Filed
May 23, 2011
0Patent Primary Examiner
Edits on 19 Jan, 2022
Golden AI
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US Patent 09908617 Active flow control for transonic flight
Infobox
Is a
Patent jurisdiction
Patent number
09908617
Date of patent
March 6, 2018
Patent application number
13114006
Date Filed
May 23, 2011
Patent primary examiner
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