High Reynolds and Mach numbers post-shock turbulence
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- Daniel Livescu
![Simulations set-up](../_assets/images/simulation-setup.jpg)
Data generated in separate IT simulations are fed through the inlet of a shock tube with a stationary shock inside.
High Reynolds and Mach numbers post-shock turbulence
In a recent shock-resolved Direct Numerical Simulations (DNS) study of the shock-turbulence interaction, we have shown that, when there is a large scale separation between turbulence scales and shock width and the upstream turbulence is weak, the interaction can be described by the Linear Interaction Approximation (LIA).