Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M2.1
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_M2.1 | 5 | 0.56688 | 1.91655 | 5 | 1.4 | 2.1 | 24.614 | 4.96616 | 1.3272 | 87.2118 | 32.605 |
| OBLIQUE_SHOCK_M2.1 | 10 | 0.58489 | 1.73251 | 10 | 1.4 | 2.1 | 24.614 | 4.92645 | 1.73423 | 84.2365 | 37.4332 |
| OBLIQUE_SHOCK_M2.1 | 15 | 0.61995 | 1.53708 | 15 | 1.4 | 2.1 | 24.614 | 4.84656 | 2.23924 | 80.7909 | 43.1434 |
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