Oblique Shock Prandtl Meyer: PRANDTL MEYER
5 to 9.5
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 | 5 | 1.4 | 5 | 11.536959 | 76.920216 |
| PRANDTL MEYER | 5.5 | 1.4 | 5.5 | 10.475682 | 81.24479 |
| PRANDTL MEYER | 6 | 1.4 | 6 | 9.594068 | 84.955498 |
| PRANDTL MEYER | 6.5 | 1.4 | 6.5 | 8.849883 | 88.168161 |
| PRANDTL MEYER | 7 | 1.4 | 7 | 8.213211 | 90.972732 |
| PRANDTL MEYER | 7.5 | 1.4 | 7.5 | 7.662256 | 93.439668 |
| PRANDTL MEYER | 8 | 1.4 | 8 | 7.180756 | 95.624672 |
| PRANDTL MEYER | 8.5 | 1.4 | 8.5 | 6.756327 | 97.572206 |
| PRANDTL MEYER | 9 | 1.4 | 9 | 6.37937 | 99.318099 |
| PRANDTL MEYER | 9.5 | 1.4 | 9.5 | 6.042328 | 100.891483 |
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