The Unsteady Shock Boundary Layer Interaction in a Compressor Cascade - Part 2: High-Fidelity Simulation - Promotional Videos

<p>Animation of high-fidelity simulation data showing the shock boundary layer interaction in a transonic compressor cascade for the ASME Turbo Expo 2024 paper "The Unsteady Shock Boundary Layer Interaction in a Compressor Cascade - Part 2: High-Fidelity Simulation" (GT2024-124264).</p> <p>The simulations were performed on the national supercomputer HPE Apollo Hawk at the High Performance Computing Center Stuttgart (HLRS) under the grant number TCTA-SBLI/44238.</p> <p>&nbsp;</p>