3D Simulation of HSCT Inlet at the Angle of Attack. The mesh resolution is 72 x 16 x 42. Shocks are extracted from the dataset.

The terminal shock is tracked and then isolated with the feature tracking algorithm. Its centroid position is computed over time.

Zooming in

Pressure Gradient

Mach

Divergence

Data range
1) -37.077 - 223.516
2) -37.387 - 225.608
3) -37.619 - 225.607
4) -29.920 - 225.607

Vorticity

Data range
1) 0.000 - 3922.750
2) 0.000 - 3965.070
3) 0.000 - 3965.060
4) 0.000 - 3965.060