Turbulence Models: Shock Boundary Layer Interaction at M=2.05

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.

Data and Resources

Additional Info

Field Value
Maintainer Christopher Rumsey
Last Updated April 1, 2025, 01:59 (UTC)
Created April 1, 2025, 01:59 (UTC)
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identifier NASA-855__2
issued 2018-06-25
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modified 2024-08-07
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publisher National Aeronautics and Space Administration
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