Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M1.9
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_M1.9 | 5 | 0.60263 | 1.72512 | 5 | 1.4 | 1.9 | 21.1675 | 4.03068 | 1.30444 | 86.6572 | 36.2288 |
| OBLIQUE_SHOCK_M1.9 | 10 | 0.62566 | 1.54641 | 10 | 1.4 | 1.9 | 21.1675 | 3.98279 | 1.68183 | 83.0195 | 41.4904 |
| OBLIQUE_SHOCK_M1.9 | 15 | 0.67363 | 1.34927 | 15 | 1.4 | 1.9 | 21.1675 | 3.87929 | 2.15893 | 78.5589 | 47.9951 |
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