Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M5.0
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_M5.0 | 5 | 0.41773 | 4.49318 | 5 | 1.4 | 5 | 41.1177 | 28.98598 | 1.80567 | 88.7439 | 15.0727 |
| OBLIQUE_SHOCK_M5.0 | 10 | 0.42546 | 3.99916 | 10 | 1.4 | 5 | 41.1177 | 28.94226 | 3.04367 | 87.4499 | 19.376 |
| OBLIQUE_SHOCK_M5.0 | 15 | 0.43914 | 3.50405 | 15 | 1.4 | 5 | 41.1177 | 28.86326 | 4.78083 | 86.0739 | 24.3217 |
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