Influence of pitching angle of incidence on the dynamic stall behavior of a symmetric airfoil

DOI10.1016/j.euromechflu.2006.07.004zbMath1154.76334OpenAlexW2022419142MaRDI QIDQ929493

Sunetra Sarkar, Kartik Venkatraman

Publication date: 17 June 2008

Published in: European Journal of Mechanics. B. Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.euromechflu.2006.07.004

zbMATH Keywords

discrete vortex techniquedynamic stall vortexperiod doubling behavior

Mathematics Subject Classification ID

Viscous vortex flows (76D17) Vortex methods applied to problems in fluid mechanics (76M23)

Related Items (1)

Identifying the route to chaos in the flow past a flapping airfoil

Cites Work

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• Discrete Vortex Method for Simulating Unsteady Flow
• Contributions to the theory of heat transfer through a laminar boundary layer
• A vorticity-based method for incompressible unsteady viscous flows

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