Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M2.0
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_M2.0 | 5 | 0.58356 | 1.82125 | 5 | 1.4 | 2 | 22.9735 | 4.48692 | 1.31541 | 86.9651 | 34.3016 |
| OBLIQUE_SHOCK_M2.0 | 10 | 0.6037 | 1.64052 | 10 | 1.4 | 2 | 22.9735 | 4.44381 | 1.70658 | 83.7001 | 39.3139 |
| OBLIQUE_SHOCK_M2.0 | 15 | 0.64397 | 1.44572 | 15 | 1.4 | 2 | 22.9735 | 4.35456 | 2.19465 | 79.8317 | 45.3436 |
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