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.
Resources
| Name | Format | Description | Link |
|---|---|---|---|
| Web Resource | xlsx | LENS2-largeconeflare.xlsx | Open resource |