Pages that link to "Item:Q2289626"
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The following pages link to Incident shock wave and supersonic turbulent boundary layer interactions near an expansion corner (Q2289626):
Displaying 11 items.
- Numerical studies of shock wave interactions with a supersonic turbulent boundary layer in compression corner:turning angle effects (Q1648233) (← links)
- Analysis of shock unsteadiness in a supersonic over-expanded planar nozzle (Q1672489) (← links)
- Anisotropic SST turbulence model for shock-boundary layer interaction (Q2245489) (← links)
- Shock wave and turbulent boundary layer interaction in a double compression ramp (Q2245514) (← links)
- DNS of Shock/Boundary Layer Interaction Flow in a Supersonic Compression Ramp (Q2822451) (← links)
- Corner separation effects for normal shock wave/turbulent boundary layer interactions in rectangular channels (Q2863274) (← links)
- Expansion wave diffraction over a 90 degree corner (Q3448451) (← links)
- Corner effects for oblique shock wave/turbulent boundary layer interactions in rectangular channels (Q4613953) (← links)
- Comparative study on single-incident and dual-incident shock wave/turbulent boundary layer interactions with identical total deflection angle (Q5068969) (← links)
- Numerical Investigation of Multiple Shock/Turbulent Flow Interaction in a Supersonic Channel (Q5156569) (← links)
- Separation length scaling for dual-incident shock wave–turbulent boundary layer interactions with different shock wave distances (Q5886410) (← links)