Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M2.2
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_M2.2 | 5 | 0.55219 | 2.01115 | 5 | 1.4 | 2.2 | 26.1028 | 5.4685 | 1.33965 | 87.4132 | 31.0971 |
| OBLIQUE_SHOCK_M2.2 | 10 | 0.56857 | 1.8228 | 10 | 1.4 | 2.2 | 26.1028 | 5.43127 | 1.76413 | 84.6697 | 35.7855 |
| OBLIQUE_SHOCK_M2.2 | 15 | 0.59988 | 1.62486 | 15 | 1.4 | 2.2 | 26.1028 | 5.35787 | 2.28999 | 81.5431 | 41.2688 |
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