Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M3.75
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_M3.75 | 5 | 0.44518 | 3.41936 | 5 | 1.4 | 3.75 | 37.9062 | 16.22883 | 1.57649 | 88.5327 | 19.0237 |
| OBLIQUE_SHOCK_M3.75 | 10 | 0.45408 | 3.09737 | 10 | 1.4 | 3.75 | 37.9062 | 16.19512 | 2.38498 | 87.0158 | 23.2268 |
| OBLIQUE_SHOCK_M3.75 | 15 | 0.46996 | 2.77034 | 15 | 1.4 | 3.75 | 37.9062 | 16.13361 | 3.45868 | 85.3903 | 28.0394 |
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