Oblique Shock Prandtl Meyer: PRANDTL MEYER
1.5 to 1.95
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 | 1.5 | 1.4 | 1.5 | 41.810315 | 11.905209 |
| PRANDTL MEYER | 1.55 | 1.4 | 1.55 | 40.17777 | 13.381214 |
| PRANDTL MEYER | 1.6 | 1.4 | 1.6 | 38.682187 | 14.860354 |
| PRANDTL MEYER | 1.65 | 1.4 | 1.65 | 37.305201 | 16.337887 |
| PRANDTL MEYER | 1.7 | 1.4 | 1.7 | 36.031879 | 17.80991 |
| PRANDTL MEYER | 1.75 | 1.4 | 1.75 | 34.849905 | 19.273192 |
| PRANDTL MEYER | 1.8 | 1.4 | 1.8 | 33.748989 | 20.725064 |
| PRANDTL MEYER | 1.85 | 1.4 | 1.85 | 32.720443 | 22.163318 |
| PRANDTL MEYER | 1.9 | 1.4 | 1.9 | 31.756864 | 23.586135 |
| PRANDTL MEYER | 1.95 | 1.4 | 1.95 | 30.851886 | 24.992021 |
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