LES of hypersonic flow over a 3D single-fin
(2015)
Presentation / Conference Contribution
LES of hypersonic flow passing a 3D single-fin at Mach 5 and Re∞=3.7×107/m was conducted using a newly developed 7th-order low-dissipation monotonicity-preserving NS solver with dynamic Smagorinsky subgrid model. The simulation captures salient flow... Read More about LES of hypersonic flow over a 3D single-fin.