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Compressible Flow: ISENTROPIC
0.92 to 1.25
Compressible flow tables — isentropic, normal shock, Fanno (friction), Rayleigh (heat addition), and Prandtl-Meyer expansion flow relations as functions of Mach number for ideal gas with gamma=1.4. Mach range 0.01 to 50.
| flow type | mach number | A Astar (dimensionless) | T T0 (dimensionless) | gamma (dimensionless) | p p0 (dimensionless) | rho rho0 (dimensionless) |
|---|---|---|---|---|---|---|
| ISENTROPIC | 0.92 | 1.005597 | 0.855227 | 1.4 | 0.578476 | 0.6764 |
| ISENTROPIC | 0.94 | 1.003108 | 0.84982 | 1.4 | 0.565775 | 0.665759 |
| ISENTROPIC | 0.96 | 1.001365 | 0.844366 | 1.4 | 0.55317 | 0.65513 |
| ISENTROPIC | 0.98 | 1.000337 | 0.83887 | 1.4 | 0.540669 | 0.64452 |
| ISENTROPIC | 1 | 1 | 0.833333 | 1.4 | 0.528282 | 0.633938 |
| ISENTROPIC | 1.05 | 1.002029 | 0.819336 | 1.4 | 0.497872 | 0.607653 |
| ISENTROPIC | 1.1 | 1.007925 | 0.805153 | 1.4 | 0.468354 | 0.581696 |
| ISENTROPIC | 1.15 | 1.017454 | 0.790826 | 1.4 | 0.439829 | 0.556164 |
| ISENTROPIC | 1.2 | 1.03044 | 0.776398 | 1.4 | 0.412377 | 0.531142 |
| ISENTROPIC | 1.25 | 1.046753 | 0.761905 | 1.4 | 0.386058 | 0.506701 |
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