Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M4.0
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_M4.0 | 5 | 0.43773 | 3.63825 | 5 | 1.4 | 4 | 38.7739 | 18.48874 | 1.61992 | 88.5926 | 18.0213 |
| OBLIQUE_SHOCK_M4.0 | 10 | 0.44629 | 3.28605 | 10 | 1.4 | 4 | 38.7739 | 18.4535 | 2.50604 | 87.1391 | 22.2341 |
| OBLIQUE_SHOCK_M4.0 | 15 | 0.46152 | 2.92901 | 15 | 1.4 | 4 | 38.7739 | 18.38939 | 3.69726 | 85.5851 | 27.0629 |
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