Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M2.4
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_M2.4 | 5 | 0.52757 | 2.19858 | 5 | 1.4 | 2.4 | 28.6814 | 6.54271 | 1.36609 | 87.721 | 28.5279 |
| OBLIQUE_SHOCK_M2.4 | 10 | 0.54165 | 1.99936 | 10 | 1.4 | 2.4 | 28.6814 | 6.50867 | 1.82918 | 85.324 | 33.0231 |
| OBLIQUE_SHOCK_M2.4 | 15 | 0.56791 | 1.79267 | 15 | 1.4 | 2.4 | 28.6814 | 6.44333 | 2.40481 | 82.6493 | 38.2137 |
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