Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M4.25
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_M4.25 | 5 | 0.43147 | 3.85506 | 5 | 1.4 | 4.25 | 39.5051 | 20.8944 | 1.66457 | 88.6414 | 17.1448 |
| OBLIQUE_SHOCK_M4.25 | 10 | 0.43976 | 3.47052 | 10 | 1.4 | 4.25 | 39.5051 | 20.85737 | 2.63244 | 87.2395 | 21.3742 |
| OBLIQUE_SHOCK_M4.25 | 15 | 0.45448 | 3.08153 | 15 | 1.4 | 4.25 | 39.5051 | 20.79015 | 3.94874 | 85.7432 | 26.2265 |
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