Test case matrix for the assessment of the base version (Legacy USM3D)

Configuration Flow/Grid type Flow Conditions Validation Quantity Validation Reference
Flat Plate Laminar 0.5 0.0 0.01 Blasius solution
Turbulent/Wall function grid 0.5 0.0 2.0 Analytical solution
RAE2822 airfoil Turbulent/Wall function grid 0.75 2.72 6.2
Cook, P. et al.
ONERA M6 Wing Turbulent/Full viscous grid 0.8447 5.06 11.7
Schmitt, V., and Charpin, E.
Turbulent/Wall function grid
NTF PathFinder Turbulent/Wall function grid 0.8199 1.9822 0.519627
Jacobs, P. F.
Generic Business Jet Turbulent/Wall function grid 0.753 .010 .0