Flow past a cylinder inside a duct

Velocity magnitude contours on the cylinder and on the lower wall

Velocity distribution on the cylinder

Velocity distribution on the lower wall

Velocity distribution along the center line of the duct

Horizontal velocity profile downstream of the cylinder

Flow past a swept wing

Pressure on a wing section close to the wing root (AoA = 3 deg)

Particle paths to visualize the tip vortex

Flow past an aircraft (wing – body – nacelle)

Pressure distribution on a wing section ( y / b = 0.4 )

Flow past a high-lift wing

Views close to the flap and the slat

Pressure distribution at the spanwise section A (AoA = 3 deg)