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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Abstract
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 |
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Publication: | Journal of Fluids and Structures |
Publisher: | Elsevier |
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: | 12 Oct 2020 11:07 |
URI: | http://eprints.iisc.ac.in/id/eprint/10108 |
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