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Review of Compressible Dynamic Stall and Its ControlA review of compressibility effects on dynamic stall of pitching airfoils and unsteady separation control by manipulation of unsteady vorticity using a deformable leading edge airfoil design is presented.
Document ID
20000101662
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Chandrasekhara, M. S. (Naval Postgraduate School Monterey, CA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1999
Subject Category
Aerodynamics
Meeting Information
Meeting: 8th Asian Congress of Fluid Mechanics
Location: Shenzhen
Country: China
Start Date: December 6, 1999
End Date: December 10, 1999
Funding Number(s)
PROJECT: RTOP 519-20-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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