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.
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Complete Metadata
| @type | dcat:Dataset |
|---|---|
| accessLevel | public |
| accrualPeriodicity | irregular |
| bureauCode |
[
"026:00"
]
|
| contactPoint |
{
"fn": "Christopher Rumsey",
"@type": "vcard:Contact",
"hasEmail": "mailto:c.l.rumsey@nasa.gov"
}
|
| description | 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. |
| identifier | NASA-850 |
| issued | 2018-06-25 |
| keyword |
[
"boundary",
"experiment",
"layer",
"mach",
"models",
"shockwave",
"turbulence",
"validation"
]
|
| landingPage | https://turbmodels.larc.nasa.gov/Other_exp_Data/cfdval2004_exp.html |
| modified | 2025-07-17 |
| programCode |
[
"026:023"
]
|
| publisher |
{
"name": "National Aeronautics and Space Administration",
"@type": "org:Organization"
}
|
| references |
[
"http://turbmodels.larc.nasa.gov/index.html"
]
|
| theme |
[
"Aerospace"
]
|
| title | Turbulence Models: Data from Other Experiments: Shock Wave / Turbulent Boundary Layer Flows at High Mach Numbers |
