Advanced Laminar Flow Control on a Swept Wing: Useful Crossflow Vortices and Suction (Invited)

Abstract

Results of high-order direct numerical simulations are summarized for the evolution of crossflow disturbances in incompressible wing-generic boundary-layers with suction at the wall. The concept of smart suction, an adapted combination of the upstream-flow-deformation (UFD) technique and suction, is presented for laminar flow control. In the UFD technique… (More)

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Cite this paper

@inproceedings{Kloker2008AdvancedLF, title={Advanced Laminar Flow Control on a Swept Wing: Useful Crossflow Vortices and Suction (Invited)}, author={Markus J. Kloker}, year={2008} }