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Fluid Mechanics of Wing Adaptation for Separation ControlThe unsteady fluid mechanics associated with use of a dynamically deforming leading edge airfoil for achieving compressible flow separation control has been experimentally studied. Changing the leading edge curvature at rapid rates dramatically alters the flow vorticity dynamics which is responsible for the many effects observed in the flow.
Document ID
20020042317
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Chandrasekhara, M. S. (Naval Postgraduate School Monterey, CA United States)
Wilder, M. C. (MCAT Inst. Mountain View, CA United States)
Carr, L. W. (NASA Ames Research Center Moffett Field, CA United States)
Davis, Sanford S.
Date Acquired
September 7, 2013
Publication Date
January 1, 1997
Subject Category
Aerodynamics
Meeting Information
Meeting: 7th Asian Congress of Fluid Mechanics
Location: Madras
Country: India
Start Date: December 8, 1997
End Date: December 12, 1997
Funding Number(s)
PROJECT: RTOP 522-31-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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