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LES of NACA0012 using high-order multiblock immersed boundary method
Large-Eddy Simulation of a NACA airfoil using an Immersed Boundary method
LES, Large Eddey Simulation, Contours Of Dynamic Pressure, NACA0012 Aerofoil
NACA 0012 at 14.6 angle of attack and 60Hz pulsing
Euler solution, NACA0012, Mach = 2.0, AoA = 0
High order LES for shock-boundary interaction!
LES of Re=1000 flow in eccentric stenosis
Pitch and stop at 13 degree (NACA 0012)
Naca0012 Schlieren
NACA 0012 Airfoil
Immersed Boundary Simulation of Unsteady Flow Around a NACA0015 Airfoil
2D Steady Turn of NACA0012 with Gerris