| # | Problem Description | Code | |
|---|---|---|---|
| 1 |  Properties behind oblique shock wave |
-- | -- |
| 2 |  Stagnation pressure ratio |
-- | -- |
| 3 |  Wedge at an angle of attack |
-- | -- |
| 4 |  Mach line and wall turn angle |
-- | -- |
| 5 |  Turning angle of corner |
-- | -- |
| 6 |  Flow pattern and attached shock limit |
-- | -- |
| 7 |  Largest wall corner angle |
-- | -- |
| 8 |  Minimum Mach number limit |
-- | -- |
| 9 |  Optical method for Mach number calculation |
-- | -- |
| 10 |  2D Shock reflection |
-- | -- |
| 11 |  Properties behind reflected shock |
-- | -- |
| 12 |  Mach reflection range |
-- | -- |
| 13 |  Two Oblique shock reflections |
-- | -- |
| 14 |  Pressure after reflection |
-- | -- |
| 15 |  Shock reflection with deflected wall |
-- | -- |
| 16 |  Shock reflection with deflected wall |
-- | -- |
| 17 |  Shock-shock intersection |
-- | -- |
| 18 |  Pressure calculation (Shock intersection) |
-- | -- |
| 19 |  Pressure calculation (Shock intersection) |
-- | -- |
| 20 |  Flow pattern after shock intersection |
-- | -- |
| 21 |  Turbo jet engine - normal vs oblique shock |
-- | -- |
| 22 |  Ram-jet engine calculation with shocks |
-- | -- |
| 23 |  Oblique shocks for flow Mach estimation |
-- | -- |