| # | Short Problem Description | Manual solution Inactive links |
Computer solution Inactive links |
|---|---|---|---|
| 1 |  Changes in p, T, ρ |
q01.pdf | q01.py |
| 2 | Speed of sound in H2, He, and N2 | q02.pdf | q02.py |
| 3 |  Speed of sound in CO2 at different temperatures |
q03.pdf | q03.py |
| 4 |  Changes in ρ, T, V across sound wave |
q04.pdf | q04.py |
| 5 |  Mach number |
q05.pdf | q05.py |
| 6 |  Mach number |
q06.pdf | q06.py |
| 7 | Speed of airplane at an altitude | q07.pdf | q07.py |
| 8 |  Supersonic wind tunnel |
q08.pdf | q08.py |
| 9 | Mach at which the airplane flies | q09.pdf | q09.py |
| 10 |  Mach number and velocity in wind tunnel |
q10.pdf | q10.py |
| 11 |  Supersonic wind tunnel |
q11.pdf | q11.py |
| 12 |  Mach number and velocity of different gas |
q12.pdf | q12.py |
| 13 | Air velocity and Mach angle (non-standard units) | q13.pdf | q13.py |
| 14 |  Mach waves from projectile |
q14.pdf | q14.py |
| 15 |  Mach number of a flying aircraft |
q15.pdf | q15.py |
| 16 |  Aircraft noise distance |
q16.pdf | q16.py |
| 17 |  Speed of a flying aircraft |
q17.pdf | q17.py |