| # | Short Problem Description | Manual solution Inactive links |
Computer solution Inactive links |
|---|---|---|---|
| 1 |  Properties behind oblique shock wave |
q01.pdf | q01.py |
| 2 |  Stagnation pressure ratio |
q02.pdf | q02.py |
| 3 |  Wedge at an angle of attack |
q03.pdf | q03.py |
| 4 |  Mach line and wall turn angle |
q04.pdf | q04.py |
| 5 |  Turning angle of corner |
q05.pdf | q05.py |
| 6 |  Flow pattern and attached shock limit |
q06.pdf | q06.py |
| 7 |  Largest wall corner angle |
q07.pdf | q07.py |
| 8 |  Minimum Mach number limit |
q08.pdf | q08.py |
| 9 |  Optical method for Mach number calculation |
q09.pdf | q09.py |
| 10 |  2D Shock reflection |
q10.pdf | q10.py |
| 11 |  Properties behind reflected shock |
q11.pdf | q11.py |
| 12 |  Mach reflection range |
q12.pdf | q12.py |
| 13 |  Two Oblique shock reflections |
q13.pdf | q13.py |
| 14 |  Pressure after reflection |
q14.pdf | q14.py |
| 15 |  Shock reflection with deflected wall |
q15.pdf | q15.py |
| 16 |  Shock reflection with deflected wall |
q16.pdf | q16.py |
| 17 |  Shock-shock intersection |
q17.pdf | q17.py |
| 18 |  Pressure calculation (Shock intersection) |
q18.pdf | q18.py |
| 19 |  Pressure calculation (Shock intersection) |
q19.pdf | q19.py |
| 20 |  Flow pattern after shock intersection |
q20.pdf | q20.py |
| 21 |  Turbo jet engine - normal vs oblique shock |
q21.pdf | q21.py |
| 22 |  Ram-jet engine calculation with shocks |
q22.pdf | q22.py |
| 23 |  Oblique shocks for flow Mach estimation |
q23.pdf | q23.py |