Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M2.3
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_M2.3 | 5 | 0.53917 | 2.10514 | 5 | 1.4 | 2.3 | 27.4541 | 5.994 | 1.35264 | 87.5804 | 29.7463 |
| OBLIQUE_SHOCK_M2.3 | 10 | 0.55427 | 1.91169 | 10 | 1.4 | 2.3 | 27.4541 | 5.95861 | 1.79587 | 85.0262 | 34.3264 |
| OBLIQUE_SHOCK_M2.3 | 15 | 0.58275 | 1.70989 | 15 | 1.4 | 2.3 | 27.4541 | 5.88987 | 2.34546 | 82.1498 | 39.6427 |
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