Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M1.6
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_M1.6 | 5 | 0.68053 | 1.42891 | 5 | 1.4 | 1.6 | 14.6515 | 2.79759 | 1.28019 | 85.031 | 44.1082 |
| OBLIQUE_SHOCK_M1.6 | 10 | 0.72502 | 1.23969 | 10 | 1.4 | 1.6 | 14.6515 | 2.71324 | 1.64303 | 79.1017 | 51.1153 |
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