Pages that link to "Item:Q3097777"
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The following pages link to The wall pressure signature of transonic shock/boundary layer interaction (Q3097777):
Displaying 8 items.
- Correction for the influence of the walls of a transonic wind tunnel (Q1264729) (← links)
- A hybrid first-order and WENO scheme for the high-resolution and computationally efficient modeling of pollutant transport (Q2245384) (← links)
- Turbulence in supersonic boundary layers at moderate Reynolds number (Q2893756) (← links)
- A spectral inspection for turbulence amplification in oblique shock wave/turbulent boundary layer interaction (Q5045206) (← links)
- Wall-cooling effects on pressure fluctuations in compressible turbulent boundary layers from subsonic to hypersonic regimes (Q5094690) (← links)
- On the turbulence amplification in shock-wave/turbulent boundary layer interaction (Q5114282) (← links)
- Effect of wall cooling on boundary-layer-induced pressure fluctuations at Mach 6 (Q5364788) (← links)
- Post-shock turbulence recovery in oblique-shock/turbulent boundary layer interaction flows (Q5888972) (← links)