Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M2.8
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_M2.8 | 5 | 0.49183 | 2.56766 | 5 | 1.4 | 2.8 | 32.5875 | 8.97005 | 1.42352 | 88.1101 | 24.6427 |
| OBLIQUE_SHOCK_M2.8 | 10 | 0.50327 | 2.33993 | 10 | 1.4 | 2.8 | 32.5875 | 8.93856 | 1.97508 | 86.1403 | 28.9402 |
| OBLIQUE_SHOCK_M2.8 | 15 | 0.52412 | 2.10648 | 15 | 1.4 | 2.8 | 32.5875 | 8.87971 | 2.6725 | 83.9895 | 33.8582 |
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