Pages that link to "Item:Q532248"
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The following pages link to Numerical investigation of the effect of winglets on the evolution of an aircraft vortex wake (Q532248):
Displaying 7 items.
- Equations of perturbation growth in aircraft wakes (Q1402773) (← links)
- Modeling the turbulent vortex wake behind a high-lift wing (Q1402819) (← links)
- Hybrid numerical technique for evaluating wing aerodynamic loading with propeller interference (Q1962730) (← links)
- Effect of incidence angle with wake passing on a film cooled leading edge: A numerical study (Q3579860) (← links)
- On numerical modelling of a three-dimensional flow past a wing with external flow suction and on the effect of flow suction on trailing vortices (Q4821637) (← links)
- Active and passive vortex wake mitigation using control surfaces (Q5491302) (← links)
- Vortex wake behind an aircraft with a high-aspect-ratio wing (Q6167784) (← links)