Feedback control of laminar flow separation on NACA23012 airfoil by POD analysis and using perturbed Navier-Stokes equations

Author:

Zare A.1ORCID,Emdad H.2,Goshtasbirad E.

Affiliation:

1. Department of Mechanical Engineering, Marvdasht Branch; Islamic Azad University; Marvdasht Iran

2. Department of Mechanical Engineering; Shiraz University; Shiraz Iran

Publisher

Wiley

Subject

Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference23 articles.

1. A vortex generator model and its application to flow control;Jirasek;AIAA Paper,2004

2. Numerical study of passive and active flow separation control over a NACA0012 airfoil;Shan;Comput Fluids,2008

3. Numerical study of blowing and suction control mechanism on NACA0012 airfoil;Huang;J Aircr,2004

4. Numerical investigation of flow control by suction and injection on a subsonic airfoil;Shojaefard;American Journal of Applied Sciences,2005

5. First stages of the transition to turbulence and control in the incompressible detached flow around a NACA0012 wing;Hoarau;International Journal of Heat and Fluid Flow,2006

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