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

This dataset has no data

Additional Info

Field	Value
Maintainer	Christopher Rumsey
Last Updated	July 17, 2025, 17:43 (UTC)
Created	April 1, 2025, 02:24 (UTC)
accessLevel	public
accrualPeriodicity	irregular
bureauCode	{026:00}
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catalog_@id	https://data.nasa.gov/data.json
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harvest_object_id	b8b7ea64-2212-43a4-9381-8c0a6d532571
harvest_source_id	61638e72-b36c-4866-9d28-551a3062f158
harvest_source_title	DNG Legacy Data
identifier	NASA-850
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
references	{http://turbmodels.larc.nasa.gov/index.html}
resource-type	Dataset
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