Publication Date:
2018-02-09
Description:
Author(s): D. De Grazia, D. Moxey, S. J. Sherwin, M. A. Kravtsova, and A. I. Ruban The boundary-layer separation produced by a small hump in a high-speed subsonic regime typical of civil aviation is studied. Different heights of the hump are considered, with the larger resulting in a fully nonlinear regime and the formation of a pair of streamwise counterrotating vortices. [Phys. Rev. Fluids 3, 024101] Published Thu Feb 08, 2018
Keywords:
Laminar and Viscous Flows
Electronic ISSN:
2469-990X
Topics:
Physics
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