Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M2.5
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_M2.5 | 5 | 0.51719 | 2.29152 | 5 | 1.4 | 2.5 | 29.7974 | 7.11465 | 1.37995 | 87.8406 | 27.4227 |
| OBLIQUE_SHOCK_M2.5 | 10 | 0.53043 | 2.08593 | 10 | 1.4 | 2.5 | 29.7974 | 7.08162 | 1.86387 | 85.5761 | 31.8506 |
| OBLIQUE_SHOCK_M2.5 | 15 | 0.55492 | 1.87353 | 15 | 1.4 | 2.5 | 29.7974 | 7.01877 | 2.4675 | 83.0673 | 36.9449 |
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