Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M2.7
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_M2.7 | 5 | 0.49945 | 2.47604 | 5 | 1.4 | 2.7 | 31.7406 | 8.32831 | 1.40869 | 88.0324 | 25.4917 |
| OBLIQUE_SHOCK_M2.7 | 10 | 0.51139 | 2.25615 | 10 | 1.4 | 2.7 | 31.7406 | 8.29649 | 1.93691 | 85.9781 | 29.8233 |
| OBLIQUE_SHOCK_M2.7 | 15 | 0.53325 | 2.03029 | 15 | 1.4 | 2.7 | 31.7406 | 8.23676 | 2.60155 | 83.7261 | 34.7858 |
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