Pages that link to "Item:Q4613962"
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The following pages link to Analysis of the two-dimensional dynamics of a Mach 1.6 shock wave/transitional boundary layer interaction using a RANS based resolvent approach (Q4613962):
Displaying 6 items.
- Low-frequency unsteadiness mechanisms in shock wave/turbulent boundary layer interactions over a backward-facing step (Q3388849) (← links)
- Identification and reconstruction of high-frequency fluctuations evolving on a low-frequency periodic limit cycle: application to turbulent cylinder flow (Q5078923) (← links)
- Low-frequency resolvent analysis of the laminar oblique shock wave/boundary layer interaction (Q5080967) (← links)
- Dynamics of strong swept-shock/turbulent-boundary-layer interactions (Q5113090) (← links)
- Transition scenario in hypersonic axisymmetrical compression ramp flow (Q5144549) (← links)
- The anisotropic graph neural network model with multiscale and nonlinear characteristic for turbulence simulation (Q6185144) (← links)