Vortex-Wake Interaction

Flow Conditions

• Flow over an rectanglar wing of AR=6 is assumed fully turblent flow beyond the chordwise station of 0.05
• Reynolds Averaged Navier-Stokes Equations with Baldwin and Lomax turbulence model is used
• Reynolds Number is 3.2 million, angle of attack os 4.46 degree and Mach Number is 0.3

Three Types of Interference-flow cases are considered

Single wing without following wing

Along-track penetration through the vortex center

Along-track penetration between vortices