Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M3.5
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_M3.5 | 5 | 0.45416 | 3.19834 | 5 | 1.4 | 3.5 | 36.867 | 14.11465 | 1.53431 | 88.458 | 20.1813 |
| OBLIQUE_SHOCK_M3.5 | 10 | 0.46349 | 2.90438 | 10 | 1.4 | 3.5 | 36.867 | 14.08217 | 2.26929 | 86.8617 | 24.384 |
| OBLIQUE_SHOCK_M3.5 | 15 | 0.48019 | 2.6053 | 15 | 1.4 | 3.5 | 36.867 | 14.02267 | 3.23307 | 85.146 | 29.1916 |
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