Fluid Mechanics of Wing Adaptation for Separation Control
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Authors
Chandrasekhara, M.S.
Wilder, M.C.
Carr, L.W.
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1997
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Abstract
The 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.
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7th Asian Congress of Fluid Mechanics, Madras, India, Dec. 8-12, 1997.
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Citation
M.S. Chandrasekhara, M.C. Wilder, and L.W. Carr, "Fluid Mechanics of Wing Adaptation for Separation Control", 7th Asian Congress of Fluid Mechanics, Madras, India, Dec. 8-12, 1997.