| # | Problem Description | Code | |
|---|---|---|---|
| 1 |  Changes in p, T, ρ |
-- | -- |
| 2 | Speed of sound in H2, He, and N2 | -- | -- |
| 3 |  Speed of sound in CO2 at different temperatures |
-- | -- |
| 4 |  Changes in ρ, T, V across sound wave |
-- | -- |
| 5 |  Mach number |
-- | -- |
| 6 |  Mach number |
-- | -- |
| 7 | Speed of airplane at an altitude | -- | -- |
| 8 |  Supersonic wind tunnel |
-- | -- |
| 9 | Mach at which the airplane flies | -- | -- |
| 10 |  Mach number and velocity in wind tunnel |
-- | -- |
| 11 |  Supersonic wind tunnel |
-- | -- |
| 12 |  Mach number and velocity of different gas |
-- | -- |
| 13 | Air velocity and Mach angle (non-standard units) | -- | -- |
| 14 |  Mach waves from projectile |
-- | -- |
| 15 |  Mach number of a flying aircraft |
-- | -- |
| 16 |  Aircraft noise distance |
-- | -- |
| 17 |  Speed of a flying aircraft |
-- | -- |