Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M1.7
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_M1.7 | 5 | 0.65022 | 1.5294 | 5 | 1.4 | 1.7 | 17.0119 | 3.18643 | 1.28623 | 85.7445 | 41.029 |
| OBLIQUE_SHOCK_M1.7 | 10 | 0.68377 | 1.34822 | 10 | 1.4 | 1.7 | 17.0119 | 3.12077 | 1.64656 | 80.9058 | 47.1668 |
| OBLIQUE_SHOCK_M1.7 | 15 | 0.76989 | 1.12207 | 15 | 1.4 | 1.7 | 17.0119 | 2.9438 | 2.14982 | 73.8392 | 55.984 |
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