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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 Open NASA

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.

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Related

Provenance · 1 source records, 6 field assertions
SourceKeyLast seenRaw
Open NASA45eeea79-c611-4231-a21b-f0b1863211a414 h agoJSON v1
FieldAssertionExtractorEvidence
created_datesource · open nasa govconnector:open_nasa_gov@1.0.0
descriptionsource · open nasa govconnector:open_nasa_gov@1.0.0/notes
license_textsource · open nasa govconnector:open_nasa_gov@1.0.0
publication_datesource · open nasa govconnector:open_nasa_gov@1.0.0
titlesource · open nasa govconnector:open_nasa_gov@1.0.0/title
updated_datesource · open nasa govconnector:open_nasa_gov@1.0.0