Abstract
A significant problem of the operation of an airfoil is the leading-edge separation occurring at high angles of attack which results in formation of a large-scale separation region, so that the lift cannot increase further with the angle of attack. It is a task to find control mechanisms which are as effective as possible to attain a higher critical angle of incidence.
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© 1999 Springer Science+Business Media Dordrecht
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Bader, V., Grosche, FR. (1999). Control of leading-edge separation from an airfoil by internal acoustic excitation and self-induced resonances. In: Meier, G.E.A., Viswanath, P.R. (eds) IUTAM Symposium on Mechanics of Passive and Active Flow Control. Fluid Mechanics and its Applications, vol 53. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-4199-4_48
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DOI: https://doi.org/10.1007/978-94-011-4199-4_48
Publisher Name: Springer, Dordrecht
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