Pages that link to "Item:Q5406602"
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The following pages link to Stabilization of a swept-wing boundary layer by distributed roughness elements (Q5406602):
Displaying 15 items.
- A local solution method for shock boundary-layer interaction on a swept wing (Q1310670) (← links)
- Adjustment of a turbulent boundary layer to a canopy of roughness elements (Q4467431) (← links)
- Control of stationary cross-flow modes in a Mach 6 boundary layer using patterned roughness (Q4559169) (← links)
- Effects of distributed roughness on crossflow instability through generalized resonance mechanisms (Q4559309) (← links)
- Control of a swept-wing boundary layer using ring-type plasma actuators (Q4563613) (← links)
- Stationary crossflow vortices near the leading edge of three-dimensional boundary layers: the role of non-parallelism and excitation by surface roughness (Q4614406) (← links)
- Mechanisms of flow tripping by discrete roughness elements in a swept-wing boundary layer (Q4976662) (← links)
- Transition in an infinite swept-wing boundary layer subject to surface roughness and free-stream turbulence (Q5014149) (← links)
- Distributed vortex receptivity of a swept-wing boundary layer. Part 1. Efficient excitation of CF modes (Q5144753) (← links)
- Conditioning of cross-flow instability modes using dielectric barrier discharge plasma actuators (Q5225996) (← links)
- Transition to turbulence in the rotating-disk boundary-layer flow with stationary vortices (Q5226197) (← links)
- Control of crossflow-vortex-induced transition by unsteady control vortices (Q5378175) (← links)
- Control of stationary cross-flow modes in a Mach 3.5 boundary layer using patterned passive and active roughness (Q5406575) (← links)
- The near wake of discrete roughness elements on swept wings (Q6488295) (← links)
- Roughness induced transition delay in a swept-wing boundary layer in presence of freestream disturbances. I: Turbulence effects (Q6546147) (← links)
