Effects of Spanwise Domain Size on LES-Predicted Aerodynamics of Stalled Airfoil
Author:
Affiliation:
1. Tohoku University, Sendai, Miyagi, 980-8579, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J062375
Reference20 articles.
1. Springer Science & Business Media;Davidson L.,2003
2. Lessons from the European LESFOIL project on LES of flow around an airfoil
3. Assessment of spanwise domain size effect on the transitional flow past an airfoil
4. Effect of spanwise domain size on direct numerical simulations of airfoil noise during flow separation and stall
5. Pade-plusmn;-Type Higher-Order Boundary Filters for the Navier-Stokes Equations
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