Turbulence Models: Data from Other Experiments: Shock Wave / Turbulent Boundary Layer Flows at High Mach Numbers

Shock Wave / Turbulent Boundary Layer Flows at High Mach Numbers. 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

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Additional Info

Field	Value
Maintainer	Christopher Rumsey
Last Updated	February 19, 2025, 09:23 (UTC)
Created	February 19, 2025, 09:23 (UTC)
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harvest_source_title	DNG Legacy Data
identifier	NASA-850__3
issued	2018-06-25
landingPage	https://turbmodels.larc.nasa.gov/Other_exp_Data/cfdval2004_exp.html
modified	2024-08-07
programCode	{026:023}
publisher	National Aeronautics and Space Administration
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