| # | Problem Description | Code | |
|---|---|---|---|
| 1 |  Velocity and Mach number |
-- | -- |
| 2 |  Convergent-divergent duct |
-- | -- |
| 3 |  Exhaust gases from a rocket engine |
-- | -- |
| 4 |  Exhaust gases from a rocket engine |
-- | -- |
| 5 |  Pressure, temperature and Mach number |
-- | -- |
| 6 |  Carbon dioxide flow |
-- | -- |
| 7 | Stagnation pressure and temperature | -- | -- |
| 8 | Helium flow | -- | -- |
| 9 | Argon flow | -- | -- |
| 10 |  Stagnation pressure and temperature |
-- | -- |
| 11 | Maximum possible velocity | -- | -- |
| 12 |  Pitot-static tube |
-- | -- |
| 13 | Pitot-static tube | -- | -- |
| 14 | Pitot tube | -- | -- |
| 15 | Pitot tube | -- | -- |
| 16 | Pitot tube (CO2) | -- | -- |
| 17 |  Isentropic flow through a duct |
-- | -- |
| 18 |  Liquid fuelled rocket |
-- | -- |
| 19 |  Flow through a duct |
-- | -- |
| 20 |  Diffuser at the intake of the engine |
-- | -- |
| 21 |  Conical diffuser |
-- | -- |
| 22 |  Thrust control |
-- | -- |
| 23 |  Imperial units |
-- | -- |
| 24 |  Highest pressure on aircraft |
-- | -- |
| 25 | Stagnation pressure and temperature | -- | -- |
| 26 |  Speed and the Mach number |
-- | -- |
| 27 |  Compressible vs incompressible |
-- | -- |
| 28 |  Imperial units |
-- | -- |
| 29 |  Rocket engine |
-- | -- |
| 30 | Mach number and the stagnation temperature | -- | -- |
| 31 |  Pipe flow |
-- | -- |
| 32 |  Exit door window failure |
-- | -- |