Application of Proper Orthogonal Decomposition Method in Unsteady Flow Field Analysis of Axial High Bypass Fan
Author:
Affiliation:
1. Mechanical Egnineering , Shanghai Jiao Tong University , NO. 800 Dongchuan Road , Shanghai 200240 , China
Abstract
Publisher
Walter de Gruyter GmbH
Subject
Aerospace Engineering
Link
https://www.degruyter.com/document/doi/10.1515/tjj-2020-0002/pdf
Reference19 articles.
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2. Holmes P, Lumley J, Berkooz G. Turbulence, coherent structures, dynamical systems and symmetry. New York: Cambridge university press, 1996.
3. Kim Y, Rockwell D. Vortex buffeting of aircraft tail: interpretation via proper orthogonal decomposition. AIAA. 2005;43:550–9.
4. Dai Q, Zhao L. Near freedom, PIV measurement and POD analysis of the airfoil wake velocity field. Hydrodyn Res Dev. 2008;23:196–203.
5. Gurka R, Liberzon A, Hetsroni G. POD of vorticity fields: a method for spatial characterization of coherent structures. Int J Heat Fluid Flow. 2006;27:416–23.
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