[Home] Archive [Resources] [History] [Contacts]

NPARC Alliance Verification and Validation Archive

Last Updated: Friday, 13-Feb-2009 09:24:54 EST

The archive consists of cases. Each case represents a geometric configuration and flow condition (i.e. ONERA M6 wing, MADIC 3D nozzle). A case can be classified as either a verification or validation case depending on whether the comparison data for the case is exact (analytical) or experimental, respectively. Each case contains one or more studies. Each study consists of one or more runs of the Wind-US code (or another CFD code). Throughout some of the cases and studies are detailed examples that provide a step-by-step description or tutorial on using WIND and associated tools.

Downloading Files from the Archive

The cases of the archive include:

NLR Airfoil with Flap

Incompressible Driven Cavity

Hypersonic Cylinder

Mach 7, Laminar 15-degree Ramp

Normal shock at Mach 1.3

Oblique shock on a 15 degree wedge at Mach 2.5

Conical shock on a 10 degree cone at Mach 2.35.

Prandtl-Meyer 15 Degree Expansion Corner at Mach 2.5.

Blasius Incompressible Laminar Flat Plate

Steady, Inviscid Flow in a Converging-Diverging Verfication (CDV) Nozzle.