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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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Нэмэлт мэдээлэл

Талбар Утга
Арчлагч Christopher Rumsey
Сүүлийн шинэчлэл 2021 3-р сар 6, 09:00 (EST)
Үүссэн 2021 3-р сар 6, 09:00 (EST)
Identifier NASA-850__4
Issued 2018-06-25
Modified 2020-01-29
Theme {Aerospace}
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publisher National Aeronautics and Space Administration
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resource-type Dataset
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