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Turbulence Models: Shock Boundary Layer Interaction at M=2.05

Published by National Aeronautics and Space Administration | National Aeronautics and Space Administration | Metadata Last Checked: October 06, 2025 | Last Modified: 2025-03-31
Exp: Shock Boundary Layer Interaction at M=2.05. This web page provides data from experiments that may be useful for the validation of turbulence models. This resource is expected to grow gradually over time. All data herein arepublicly available.

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