Pages that link to "Item:Q1647172"
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The following pages link to Numerical study of airfoil stall cells using a very wide computational domain (Q1647172):
Displaying 11 items.
- Direct numerical simulation of flow separation around NACA 0012 airfoil (Q849726) (← links)
- Numerical analysis on the oscillation of stall cells over a NACA 0012 aerofoil (Q1615628) (← links)
- Assessment of spanwise domain size effect on the transitional flow past an airfoil (Q1646693) (← links)
- Numerical simulation of a vertical axis wind turbine airfoil experiencing dynamic stall at high Reynolds numbers (Q1648224) (← links)
- Computational study into the flow field developed around a cascade of NACA 0012 airfoils (Q1808127) (← links)
- High-fidelity modeling of turbulent shear flow downstream of a 3-D airfoil with spanwise ice contamination leading stall (Q2083891) (← links)
- Computational fluid dynamics simulation of aerodynamic performance and flow separation by single element and slatted airfoils under rainfall conditions (Q2183006) (← links)
- Link between subsonic stall and transonic buffet on swept and unswept wings: from global stability analysis to nonlinear dynamics (Q5144755) (← links)
- Bifurcation scenario for a two-dimensional static airfoil exhibiting trailing edge stall (Q5157339) (← links)
- Time-resolved topology of turbulent boundary layer separation over the trailing edge of an airfoil (Q5221405) (← links)
- Linear stability analysis of turbulent mean flows based on a data-consistent Reynolds-averaged Navier-Stokes model: prediction of three-dimensional stall cells around an airfoil (Q6661474) (← links)
