Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M1.5
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 | 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_M1.5 | 5 | 0.71723 | 1.3253 | 5 | 1.4 | 1.5 | 12.1127 | 2.42955 | 1.27798 | 83.9894 | 47.8893 |
| OBLIQUE_SHOCK_M1.5 | 10 | 0.78542 | 1.11438 | 10 | 1.4 | 1.5 | 12.1127 | 2.30459 | 1.66619 | 75.9949 | 56.6787 |
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