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 are presented and, if available, comparison with numerical data from other CFD codes and experimental data are provided.




Mach Description


Sod's Shock Tube (E)
4.5
Flow over a flat plate (NS)
3.0
Mach 3.0 windtunnel with step (E)
0.73
RAE 2822 Transonic Airfoil (NS)
0.74
ONERA M6 Wing (NS)
0.8
AGARD model B (NS)
0.5-4.5
Basic finner (NS)
0.6-2.5
Modified basic finner (NS)

Aeroelastic validation




Mach Description

0.49-1.14
AGARD 445.6 (E)