Zhengfei Guo

Swept-wing boundary-layer receptivity to free-stream vortical disturbances

Abstract Content of image described in text. Direct numerical simulations are performed to investigate the receptivity of a swept-wing boundary layer to unsteady free-stream vortical disturbances in the nose region of the airfoil. An infinite wing with a sweep angle of 35 Superscript ring ∘ $^\circ$ and at free-stream...