Pages that link to "Item:Q3532063"
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The following pages link to The effect of Mach number on unstable disturbances in shock/boundary-layer interactions (Q3532063):
Displaying 12 items.
- Direct numerical simulation of a turbulent flow over an axisymmetric Hill (Q1641328) (← links)
- Parallel Navier-Stokes simulations for high speed compressible flow past arbitrary geometries using FLASH (Q1645598) (← links)
- Numerical study of chemically reacting flow in a shock tube using a high-order point-implicit scheme (Q1739805) (← links)
- Effect of turbulent Mach number on the thermodynamic fluctuations in canonical shock-turbulence interaction (Q2285526) (← links)
- First-mode-induced nonlinear breakdown in a hypersonic boundary layer (Q2331853) (← links)
- High-speed laminar flow past a fin-body junction (Q2878579) (← links)
- Instability and low-frequency unsteadiness in a shock-induced laminar separation bubble (Q2973656) (← links)
- Disturbance evolution in a Mach 4.8 boundary layer with two-dimensional roughness-induced separation and shock (Q3573250) (← links)
- Linear, nonlinear and transitional regimes of second-mode instability (Q5131440) (← links)
- Hypersonic compression corner flow with large separated regions (Q5235642) (← links)
- Nonlinear interaction model of subsonic jet noise (Q5504019) (← links)
- Interactions between vortical, acoustic and thermal components during hypersonic transition (Q5742310) (← links)
