This is a simple 2D-airfoil CFD case using OpenFOAM v10. Only use for study and research.
Mesh ( From curiosityFluidsAirfoilMesher )
CL v AOA
CD v AOA
CM v AOA
CL v CD
Ma=0.2, AOA=14°
Ma=0.4, AOA=5°
Ma=0.6, AOA=25°
Ma=0.8, AOA=20°
This is a simple 2D-airfoil CFD case using OpenFOAM v10. Only use for study and research.
CL v AOA
CD v AOA
CM v AOA
CL v CD
Ma=0.2, AOA=14°
Ma=0.4, AOA=5°
Ma=0.6, AOA=25°
Ma=0.8, AOA=20°