Tangential synthetic jets for separation control
A numerical study of separation control has been made to investigate aerodynamic characteristics of a NACA23012 airfoil with a tangential synthetic jet. Simulations are carried out at the chord Reynolds number of Re=2.19×106. The present approach relies on solving the Unsteady Reynolds-Averaged Navi...
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Published in | Journal of fluids and structures Vol. 45; pp. 50 - 65 |
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Main Authors | , , |
Format | Journal Article |
Language | English |
Published |
Elsevier Ltd
01.02.2014
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Subjects | |
Online Access | Get full text |
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