| # | Problem Description | Code | |
|---|---|---|---|
| 1 |  Mach number, pressure, temperature behind expansion waves |
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| 2 |  Oblique shock and expansion waves |
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| 3 |  Expansion wave reflection |
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| 4 |  Expansion wave reflection |
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| 5 |  Expansion wave angles and pressure drop |
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| 6 |  Expansion and oblique shock wave |
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| 7 |  Expansion wave reflected off a free boundary |
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| 8 |  Expansion waves interacting with each other |
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| 9 |  Supersonic flow over symmetric double-wedge shaped body |
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| 10 |  Lift and drag of a wing modeled as flat plate |
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| 11 |  Lift and drag acting on the airfoil |
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| 12 |  Lift acting on the airfoil |
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| 13 |  Properties in the flow over a wall with bump |
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| 14 |  Oblique shock waves and maximum turning angle |
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| 15 |  Angle of a thin flat plate |
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| 16 |  Rupture of safety diaphragm |
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| 17 |  Velocity, Mach number induced by unsteady expansion wave |
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| 18 |  Valves at inlet and exit simultaneously closed |
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| 19 |  Valves at inlet and exit closed |
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| 20 |  End of the tube suddenly opened |
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| 21 |  Diaphragm suddenly ruptures |
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| 22 |  Shock tube |
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| 23 |  Shock tube |
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