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 e Risorse

Campo Valore
accessLevel public
accrualPeriodicity irregular
bureauCode {026:00}
catalog_@context https://project-open-data.cio.gov/v1.1/schema/catalog.jsonld
catalog_@id https://data.nasa.gov/data.json
catalog_conformsTo https://project-open-data.cio.gov/v1.1/schema
catalog_describedBy https://project-open-data.cio.gov/v1.1/schema/catalog.json
identifier NASA-850
issued 2018-06-25
landingPage http://cfdval2004.larc.nasa.gov/results.html
modified 2020-01-29
programCode {026:023}
publisher National Aeronautics and Space Administration
references {http://turbmodels.larc.nasa.gov/index.html}
resource-type Dataset
source_datajson_identifier true
source_hash 5089314f9a8f5c2121595cc8284893d64a5bb46d
source_schema_version 1.1
theme {Aerospace}
Gruppi
  • AmeriGEOSS
  • National Provider
  • North America
Tag
  • amerigeo
  • amerigeoss
  • boundary
  • ckan
  • experiment
  • geo
  • geoss
  • layer
  • mach
  • models
  • national
  • north-america
  • shockwave
  • turbulence
  • united-states
  • validation
isopen False
license_id notspecified
license_title License not specified
maintainer Christopher Rumsey
maintainer_email c.l.rumsey@nasa.gov
metadata_created 2025-11-22T02:20:22.034492
metadata_modified 2025-11-22T02:20:22.034496
notes 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.
num_resources 1
num_tags 16
title Turbulence Models: Data from Other Experiments: Shock Wave / Turbulent Boundary Layer Flows at High Mach Numbers