Pages that link to "Item:Q416589"
From MaRDI portal
The following pages link to Numerical study of passive and active flow separation control over a NACA0012 airfoil (Q416589):
Displaying 11 items.
- A complementary numerical and experimental study of the influence of Reynolds number on theoretical models for wingtip vortices (Q667400) (← links)
- Passive flow control of a stalled airfoil using an oscillating micro-cylinder (Q1626376) (← links)
- Assessment of spanwise domain size effect on the transitional flow past an airfoil (Q1646693) (← links)
- Numerical study on closed-loop control of transonic buffet suppression by trailing edge flap (Q1646932) (← links)
- Comparative study of boundary layer control around an ordinary airfoil and a high lift airfoil with secondary blowing (Q1649639) (← links)
- Lyapunov spectrum of the separated flow around the NACA 0012 airfoil and its dependence on numerical discretization (Q1699034) (← links)
- Performance of transition model for predicting low \(Re\) aerofoil flows without/with single and simultaneous blowing and suction (Q1940502) (← links)
- On the large-eddy simulations for the flow around aerodynamic profiles using unstructured grids (Q2015943) (← links)
- Energy efficient active control of the flow past an aircraft wing: RANS and LES evaluation (Q2289961) (← links)
- Three-dimensional suction flow control and suction jet length optimization of NACA 0012 wing (Q2356415) (← links)
- Numerical Study of the Installed Controlled Diffusion Airfoil at Transitional Reynolds Number (Q2958811) (← links)
