Input-output reduced-order modeling of unsteady flow over an airfoil at a high angle of attack based on dynamic mode decomposition with control

Author:

Sun Chong,Tian Tian,Zhu Xiaocheng,Du Zhaohui

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference26 articles.

1. State-space model identification and feedback control of unsteady aerodynamic forces;Brunton;J. Fluids Struct.,2014

2. Closed-loop turbulence control: progress and challenges;Brunton;Appl. Mech. Rev.,2015

3. Proper orthogonal decomposition and low-dimensional models for driven cavity flows;Cazemier;Phys. Fluids,1998

4. A data-driven modeling framework for predicting forces and pressures on a rapidly pitching airfoil[C]//45th AIAA;Dawson;Fluid Dynamics Conference.,2015

5. Eigenmode analysis in unsteady aerodynamics-reduced-order models;Dowell;AIAA J.,1996

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