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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1_Holden_AIAA_Atlanta_SWTBI.pdf
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Талбар	Утга
Арчлагч	Christopher Rumsey
Сүүлийн шинэчлэл	2021 3-р сар 6, 01:37 (EST)
Үүссэн	2021 3-р сар 6, 01:37 (EST)
Identifier	NASA-850__1
Issued	2018-06-25
Modified	2020-01-29
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