CFD Verification and Validation archive
This site aims to provide an archive of examples, verification and validation cases for the High Speed Aerodynamic solver (HiSA). For each of the test cases, an overview of the configuration and flow parameters are provided. A summary of the results is presented and, if available, comparison with numerical data from other CFD codes and experimental data is provided.
| Mach | Description |
Comments |
|
| Sod's
Shock Tube |
Euler; Transient; 1D | ||
| 4.5 |
Flow
over a flat plate |
Navier Stokes; Steady; 2D | |
| 3.0 |
Mach
3.0 windtunnel with step |
Euler; Transient; 2D | |
| 0.73 |
RAE
2822 Transonic Airfoil |
Navier Stokes; Steady; 2D | |
| 0.74 |
ONERA
M6 Wing |
Navier Stokes; Steady; 3D | |
| 0.8 |
AGARD
model B |
Navier Stokes; Steady; 3D | |
| 0.5-4.5 |
Basic finner |
Navier Stokes; Steady; 3D | |
| 0.6-2.5 |
Modified basic finner |
Navier Stokes; Steady; 3D | |
| 0.49-1.14 |
AGARD
445.6 |
Euler; Steady with adaptive mesh refinement; Transient with moving mesh; 3D; Modal solid modelling; Aeroelastic |