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Data · dataset · 2025

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

Listed in NASA Data Portal

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

Description

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.

Links

Related

Provenance · 1 source records, 6 field assertions
SourceKeyLast seenRaw
NASA Data Portal46f748a6-9281-40fb-a927-abbd5bd1829a10 d agoJSON v1
FieldAssertionExtractorEvidence
created_datesource · data nasa govconnector:data_nasa_gov@1.0.0
descriptionsource · data nasa govconnector:data_nasa_gov@1.0.0/notes
license_textsource · data nasa govconnector:data_nasa_gov@1.0.0
publication_datesource · data nasa govconnector:data_nasa_gov@1.0.0
titlesource · data nasa govconnector:data_nasa_gov@1.0.0/title
updated_datesource · data nasa govconnector:data_nasa_gov@1.0.0