Pages that link to "Item:Q1430085"

The following pages link to Direct numerical simulation of the three-dimensional transition to turbulence in the transonic flow around a wing (Q1430085):

Displaying 9 items.

• Organised modes and shock--vortex interaction in unsteady viscous transonic flows around an aerofoil. I: Mach number effect. (Q1415742) (← links)
• Direct numerical simulation of the three-dimensional transition to turbulence in the incompressible flow around a wing (Q1430076) (← links)
• The 3D transition to turbulence in wake flows by means of direct numerical simulation (Q1582603) (← links)
• Comprehensive mesh study for a direct numerical simulation of the transonic flow at \(\mathrm{Re}_{c} = 500,000\) around a NACA 0012 airfoil (Q1646023) (← links)
• Numerical study of the turbulent transonic interaction and transition location effect involving optimisation around a supercritical aerofoil (Q1671459) (← links)
• Three-dimensional suction flow control and suction jet length optimization of NACA 0012 wing (Q2356415) (← links)
• Direct numerical simulation of complete transition to turbulence via oblique breakdown at Mach 3 (Q2891527) (← links)
• Organized modes and the three-dimensional transition to turbulence in the incompressible flow around a NACA0012 wing (Q4467901) (← links)
• Capturing transition features around a wing by reduced-order modeling based on compressible Navier–Stokes equations (Q5304809) (← links)