Computational Modeling for the Flow Over a Multi-Element Airfoil
Computational Modeling for the Flow Over a Multi-Element Airfoil
- New search for: Liou, William W.
- New search for: Liu, Feng-Jun
- New search for: Liou, William W.
- New search for: Liu, Feng-Jun
The flow over a multi-element airfoil is computed using two two-equation turbulence models. The computations are performed using the INS2D) Navier-Stokes code for two angles of attack. Overset grids are used for the three-element airfoil. The computed results are compared with experimental data for the surface pressure, skin friction coefficient, and velocity magnitude. The computed surface quantities generally agree well with the measurement. The computed results reveal the possible existence of a mixing-layer-like region of flow next to the suction surface of the slat for both angles of attack.
Document information
Computational Modeling for the Flow Over a Multi-Element Airfoil
AIAA 17th Applied Aerodynamics Conference ; 1999 ; Norfolk, VA, United States
1999-01-01
Preprint
No indication
English
Similar titles
Computational study of flow over generic fan-wing airfoil
| Emerald Group Publishing | 2007
Computational study of flow over generic fan-wing airfoil
| Online Contents | 2007