Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M2.6
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 | M2 strong (dimensionless) | M2 weak (dimensionless) | deflection angle deg (deg) | gamma (dimensionless) | mach number (dimensionless) | max deflection angle deg (deg) | p2 over p1 strong (dimensionless) | p2 over p1 weak (dimensionless) | strong shock angle deg (deg) | weak shock angle deg (deg) |
|---|---|---|---|---|---|---|---|---|---|---|---|
| OBLIQUE_SHOCK_M2.6 | 5 | 0.50786 | 2.384 | 5 | 1.4 | 2.6 | 30.8137 | 7.70984 | 1.39416 | 87.9433 | 26.4148 |
| OBLIQUE_SHOCK_M2.6 | 10 | 0.5204 | 2.1715 | 10 | 1.4 | 2.6 | 30.8137 | 7.67753 | 1.89981 | 85.7918 | 30.7892 |
| OBLIQUE_SHOCK_M2.6 | 15 | 0.54345 | 1.95268 | 15 | 1.4 | 2.6 | 30.8137 | 7.6165 | 2.53316 | 83.422 | 35.8092 |
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