Shock Wave/Turbulent Boundary Layer Interactions

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Uploaded by on Jul 27, 2011

The design and analysis of supersonic relative flow turbomachinery needed in Carbon Capture and Storage requires computational and analysis tools that have been validated against experimental results that exhibit the same complex phenomena seen in these devices. This work demonstrates the results of one simulation conducted on a highly refined grid that resolves the 3D separation caused by crossing shocks. The video is an example of visualizations done to support this project. By M. Matheson, A. Grosvenor, and A. Zheltovodov.

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Science & Technology

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