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

Metadata Updated: November 12, 2020

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.

Access & Use Information

Public: This dataset is intended for public access and use. License: No license information was provided. If this work was prepared by an officer or employee of the United States government as part of that person's official duties it is considered a U.S. Government Work.

Downloads & Resources

References

http://turbmodels.larc.nasa.gov/index.html

Dates

Metadata Created Date November 12, 2020
Metadata Updated Date November 12, 2020
Data Update Frequency irregular

Metadata Source

Harvested from NASA Data.json

Additional Metadata

Resource Type Dataset
Metadata Created Date November 12, 2020
Metadata Updated Date November 12, 2020
Publisher National Aeronautics and Space Administration
Unique Identifier Unknown
Maintainer
Identifier NASA-850
Data First Published 2018-06-25
Data Last Modified 2020-01-29
Category Aerospace
Public Access Level public
Data Update Frequency irregular
Bureau Code 026:00
Metadata Context https://project-open-data.cio.gov/v1.1/schema/catalog.jsonld
Metadata Catalog ID https://data.nasa.gov/data.json
Schema Version https://project-open-data.cio.gov/v1.1/schema
Catalog Describedby https://project-open-data.cio.gov/v1.1/schema/catalog.json
Homepage URL http://cfdval2004.larc.nasa.gov/results.html
Program Code 026:023
Related Documents http://turbmodels.larc.nasa.gov/index.html
Source Datajson Identifier True
Source Hash 5089314f9a8f5c2121595cc8284893d64a5bb46d
Source Schema Version 1.1

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