Oblique Shock Prandtl Meyer: PRANDTL MEYER
2 to 2.45
Oblique shock wave angles and Prandtl-Meyer expansion function for supersonic and hypersonic flow. Covers two record types: (1) PRANDTL_MEYER — nu(M) expansion angle and Mach angle mu(M) for Mach 1.0–10.0; (2) OBLIQUE_SHOCK — weak and strong shock angles, downstream Mach number, and pressure ratio for each (M1, deflection angle) combination, Mach 1.0–10.0, deflection angles 5–40 degrees. gamma=1.4 throughout.
| flow type | sort key num | gamma (dimensionless) | mach number (dimensionless) | mu deg (deg) | nu deg (deg) |
|---|---|---|---|---|---|
| PRANDTL MEYER | 2 | 1.4 | 2 | 30 | 26.379761 |
| PRANDTL MEYER | 2.05 | 1.4 | 2.05 | 29.196404 | 27.748374 |
| PRANDTL MEYER | 2.1 | 1.4 | 2.1 | 28.43689 | 29.097081 |
| PRANDTL MEYER | 2.15 | 1.4 | 2.15 | 27.717748 | 30.425275 |
| PRANDTL MEYER | 2.2 | 1.4 | 2.2 | 27.035692 | 31.732496 |
| PRANDTL MEYER | 2.25 | 1.4 | 2.25 | 26.3878 | 33.01841 |
| PRANDTL MEYER | 2.3 | 1.4 | 2.3 | 25.771462 | 34.282794 |
| PRANDTL MEYER | 2.35 | 1.4 | 2.35 | 25.184337 | 35.525518 |
| PRANDTL MEYER | 2.4 | 1.4 | 2.4 | 24.624318 | 36.746531 |
| PRANDTL MEYER | 2.45 | 1.4 | 2.45 | 24.089506 | 37.945854 |
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