Identification of coherent structures in the flow past a NACA0012 airfoil via proper orthogonal decomposition
Author:
Affiliation:
1. Department of Energy, School of Mechanical Engineering, University of Campinas, 13083-860 Campinas, SP, Brazil
Funder
MCTI | Conselho Nacional de Desenvolvimento Científico e Tecnológico
Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
http://aip.scitation.org/doi/pdf/10.1063/1.4997202
Reference38 articles.
1. Computation of Trailing-Edge Flow and Noise Using Large-Eddy Simulation
2. T. F. Brooks, D. S. Pope, and M. A. Marcolini, “Airfoil self-noise and prediction,” Technical Report 1218, NASA Reference Publication, 1989.
3. Effects of trailing edge bluntness on airfoil tonal noise at low Reynolds numbers
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