Oblique Shock Prandtl Meyer: PRANDTL_MEYER
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 | gamma (dimensionless) | mach number (dimensionless) | mu deg (deg) | nu deg (deg) |
|---|---|---|---|---|---|
| PRANDTL_MEYER | 1 | 1.4 | 1 | 90 | 0 |
| PRANDTL_MEYER | 1.05 | 1.4 | 1.05 | 72.24721 | 0.487411 |
| PRANDTL_MEYER | 1.1 | 1.4 | 1.1 | 65.380023 | 1.336201 |
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