Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M1.8
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_M1.8 | 5 | 0.62461 | 1.62795 | 5 | 1.4 | 1.8 | 19.1833 | 3.59728 | 1.29458 | 86.2636 | 38.444 |
| OBLIQUE_SHOCK_M1.8 | 10 | 0.65179 | 1.44944 | 10 | 1.4 | 1.8 | 19.1833 | 3.54243 | 1.66111 | 82.1281 | 44.0567 |
| OBLIQUE_SHOCK_M1.8 | 15 | 0.71239 | 1.24452 | 15 | 1.4 | 1.8 | 19.1833 | 3.41497 | 2.13797 | 76.7573 | 51.3365 |
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