Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M2.9
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_M2.9 | 5 | 0.48491 | 2.65888 | 5 | 1.4 | 2.9 | 33.3626 | 9.63509 | 1.43862 | 88.1785 | 23.859 |
| OBLIQUE_SHOCK_M2.9 | 10 | 0.49592 | 2.42286 | 10 | 1.4 | 2.9 | 33.3626 | 9.60376 | 2.01428 | 86.2826 | 28.1296 |
| OBLIQUE_SHOCK_M2.9 | 15 | 0.5159 | 2.18132 | 15 | 1.4 | 2.9 | 33.3626 | 9.54547 | 2.74586 | 84.2195 | 33.0133 |
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