Oblique Shock Prandtl Meyer: PRANDTL MEYER
2.5 to 2.95
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 | 2.5 | 1.4 | 2.5 | 23.578178 | 39.123564 |
| PRANDTL MEYER | 2.55 | 1.4 | 2.55 | 23.088772 | 40.279791 |
| PRANDTL MEYER | 2.6 | 1.4 | 2.6 | 22.619865 | 41.414708 |
| PRANDTL MEYER | 2.65 | 1.4 | 2.65 | 22.170157 | 42.528523 |
| PRANDTL MEYER | 2.7 | 1.4 | 2.7 | 21.738461 | 43.621478 |
| PRANDTL MEYER | 2.75 | 1.4 | 2.75 | 21.323686 | 44.693837 |
| PRANDTL MEYER | 2.8 | 1.4 | 2.8 | 20.924832 | 45.74589 |
| PRANDTL MEYER | 2.85 | 1.4 | 2.85 | 20.540978 | 46.777941 |
| PRANDTL MEYER | 2.9 | 1.4 | 2.9 | 20.171271 | 47.790312 |
| PRANDTL MEYER | 2.95 | 1.4 | 2.95 | 19.814928 | 48.783333 |
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