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

Published by National Aeronautics and Space Administration | National Aeronautics and Space Administration | Metadata Last Checked: November 04, 2025 | Last Modified: 2025-07-17

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.

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Complete Metadata

bureauCode	[ "026:00" ]
identifier	NASA-850__3
issued	2018-06-25
landingPage	https://turbmodels.larc.nasa.gov/Other_exp_Data/cfdval2004_exp.html
programCode	[ "026:023" ]
references	[ "http://turbmodels.larc.nasa.gov/index.html" ]
theme	[ "Aerospace" ]