Direct Numerical Simulation of Hypersonic Boundary Layer Transition in a Digital Wind Tunnel at Mach 8
AIAA SciTech Forum ; 2021 ; Nashville, TN, US
Conference paper
No indication
English
HYPERSONIC BOUNDARY-LAYER TRANSITION EXPERIMENTS IN A MACH-6 QUIET TUNNEL
British Library Conference Proceedings | 2010
|Boundary layer transition at hypersonic Mach numbers.
NTRS | 1967
|