This grouping contains more recent incompressible-flow cases.

This grouping contains the compressible-flow cases from the 1980-81 Data Library.

This grouping contains the incompressible-flow cases from the 1980-81 Data Library.

This grouping contains the incompressible-flow cases from the 1980-81 Data Library.

This grouping contains the compressible-flow cases from the 1980-81 Data Library.

Exp: Shock Boundary Layer Interaction at M=2.05. This web page provides data from experiments that may be useful for the validation of turbulence models. This resource is...

This grouping contains the compressible-flow cases from the 1980-81 Data Library.

This grouping contains more recent compressible-flow cases.

This web page gives detailed information on the equations for various forms of the Nut-92 one-equation turbulence model.

This grouping contains the incompressible-flow cases from the 1980-81 Data Library.

This grouping contains the incompressible-flow cases from the 1980-81 Data Library.

This grouping contains the incompressible-flow cases from the 1980-81 Data Library.

This grouping contains the compressible-flow cases from the 1980-81 Data Library.

CFD Validation of Synthetic Jets and Turbulent Separation Control. This web page provides data from experiments that may be useful for the validation of turbulence models. This...

The sonic data within the building array is composed of 26 days of 30-minute average data from 30 sonic anemometers. The unobstructed tower sonic data is also the same, but of...

This grouping contains the incompressible-flow cases from the 1980-81 Data Library.

This grouping contains the compressible-flow cases from the 1980-81 Data Library.

Exp: FAITH Hill 3-D Separated Flow. This web page provides data from experiments that may be useful for the validation of turbulence models. This resource is expected to grow...

2-D Coanda Airfoil with Tangential Wall Jet. This web page provides data from experiments that may be useful for the validation of turbulence models. This resource is expected...

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...