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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Bibliographic Details
Published inJournal of fluids and structures Vol. 45; pp. 50 - 65
Main Authors Esmaeili Monir, H., Tadjfar, M., Bakhtian, A.
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.02.2014
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