DNS for flow separation control around an airfoil by pulsed jets
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Publication:993849
DOI10.1016/J.COMPFLUID.2006.10.001zbMath1194.76250OpenAlexW2048053512MaRDI QIDQ993849
Shutian Deng, Li Jiang, Chaoqun Liu
Publication date: 16 September 2010
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.compfluid.2006.10.001
Finite difference methods applied to problems in fluid mechanics (76M20) Flow control and optimization for compressible fluids and gas dynamics (76N25)
Related Items (5)
Assessment of spanwise domain size effect on the transitional flow past an airfoil ⋮ Comparative study of boundary layer control around an ordinary airfoil and a high lift airfoil with secondary blowing ⋮ Performance of transition model for predicting low \(Re\) aerofoil flows without/with single and simultaneous blowing and suction ⋮ Stability and receptivity characteristics of a laminar separation bubble on an aerofoil ⋮ Three-dimensional suction flow control and suction jet length optimization of NACA 0012 wing
Cites Work
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- Direct numerical simulation of flow separation around NACA 0012 airfoil
- Compact finite difference schemes with spectral-like resolution
- Large-eddy simulation of boundary-layer separation and transition at a change of surface curvature
- Implicit Navier-Stokes Solver for Three-Dimensional Compressible Flows
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