Some recent results regarding the global dynamical behaviour of the wake of circular cylinders and airfoils with massive separation are reviewed in this paper. In order to investigate the effect of interference, the three-dimensional instability modes are analysed for the flow around two circular cylinders in tandem. In the same way, the flow around a stalled airfoil is investigated in order to provide a better understanding of the three-dimensional characteristics of wakes forming downstream of a lifting body with massive separation. These results are compared with those found for an isolated cylinder. Some fundamental differences among these flows are discussed. (C) 2011 Elsevier Ltd. All rights reserved.
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Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, EnglandUniv London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, England
Carmo, B. S.
;
Meneghini, J. R.
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Univ Sao Paulo, Dept Mech Engn, NDF, BR-05508900 Sao Paulo, BrazilUniv London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, England
Meneghini, J. R.
;
Sherwin, S. J.
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Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, EnglandUniv London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, England
机构:
Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, EnglandUniv London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, England
Carmo, B. S.
;
Meneghini, J. R.
论文数: 0引用数: 0
h-index: 0
机构:
Univ Sao Paulo, Dept Mech Engn, NDF, BR-05508900 Sao Paulo, BrazilUniv London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, England
Meneghini, J. R.
;
Sherwin, S. J.
论文数: 0引用数: 0
h-index: 0
机构:
Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, EnglandUniv London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, England