Oblique Shock Prandtl Meyer: OBLIQUE_SHOCK_M3.0
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_M3.0 | 5 | 0.4786 | 2.74971 | 5 | 1.4 | 3 | 34.0734 | 10.32342 | 1.45398 | 88.2389 | 23.1333 |
| OBLIQUE_SHOCK_M3.0 | 10 | 0.48924 | 2.505 | 10 | 1.4 | 3 | 34.0734 | 10.29212 | 2.05447 | 86.4083 | 27.3827 |
| OBLIQUE_SHOCK_M3.0 | 15 | 0.50848 | 2.2549 | 15 | 1.4 | 3 | 34.0734 | 10.23412 | 2.82156 | 84.4217 | 32.2404 |
This is a sample. Search the full oblique shock prandtl meyer dataset and 300+ more by creating a free account and accessing the database.
Get started for FREE