Song Fu

Attachment-line turbulent boundary layer over a swept leading edge at Mach 6: Simulation and flow physics

Direct numerical simulations (DNS) are performed to investigate the spatial evolution of a three-dimensional (3-D) turbulent boundary layer over a swept blunt leading edge at freestream Mach number upper M Subscript normal infinity Baseline equals 6.0 M ∞ = 6.0 $M_\infty =6.0$ an...