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Experimental Investigation of a 2D Supercritical Circulation-Control Airfoil Using Particle Image VelocimetryRecent efforts in extreme short takeoff and landing aircraft configurations have renewed the interest in circulation control wing design and optimization. The key to accurately designing and optimizing these configurations rests in the modeling of the complex physics of these flows. This paper will highlight the physics of the stagnation and separation regions on two typical circulation control airfoil sections.
Document ID
20060022521
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Jones, Gregory S. (NASA Langley Research Center Hampton, VA, United States)
Yao, Chung-Sheng (NASA Langley Research Center Hampton, VA, United States)
Allan, Brian G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2006
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2006-3009
Meeting Information
Meeting: 3rd AIAA Flow Control Conference
Location: San Francisco, CA
Country: United States
Start Date: June 5, 2006
End Date: June 8, 2006
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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