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physics.flu-dyn2025
A Kinetic Study of Hypersonic Boundary Layer Second Mack Mode Instabilities
Mert Senkardesler, Irmak T. Karpuzcu, Deborah A. Levin +1
A flat-plate laminar boundary layer is simulated at a free stream Mach number of 6 and unit Reynolds number m using the Direct Simulation Monte C…
physics.flu-dyn2025★ 5 cited
Biglobal resolvent analysis of separated flow over a NACA0012 airfoil
Laura Victoria Rolandi, Luke Smith, Michael Amitay +2
The effects of Reynolds number across , , , and on separated flow over a two-dimensional NACA0012 airfoil at an angle of attack of are inv…