Sarkar, S and Venkatraman, K (2004) Model order reduction of unsteady flow past oscillating airfoil cascades. In: Journal of Fluids and Structures, 19 (2). pp. 239-247.
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This study focuses on developing reduced-order models for unsteady aerodynamic flows past a cascade of two-dimensional airfoils. A reduction method known as System Equivalent Reduction Expansion Process (SEREP) is used. The computational efficiency of the SEREP reduced-order model is compared with a reduced-order model formed using the Proper Orthogonal Decomposition (POD) technique. The present study shows that the SEREP is computationally more efficient than POD.
|Item Type:||Journal Article|
|Additional Information:||Copyright of this article belongs to Elsevier.|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||16 Mar 2007|
|Last Modified:||19 Sep 2010 04:35|
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