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Compressible Flow: ISENTROPIC
0.52 to 0.7
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 | 0.52 | 1.303388 | 0.948695 | 1.4 | 0.831654 | 0.876629 |
| ISENTROPIC | 0.54 | 1.270321 | 0.944894 | 1.4 | 0.82005 | 0.867876 |
| ISENTROPIC | 0.56 | 1.240294 | 0.940982 | 1.4 | 0.808228 | 0.85892 |
| ISENTROPIC | 0.58 | 1.213007 | 0.936961 | 1.4 | 0.796206 | 0.849775 |
| ISENTROPIC | 0.6 | 1.1882 | 0.932836 | 1.4 | 0.784004 | 0.840452 |
| ISENTROPIC | 0.62 | 1.165646 | 0.928609 | 1.4 | 0.771639 | 0.830963 |
| ISENTROPIC | 0.64 | 1.145148 | 0.924283 | 1.4 | 0.759131 | 0.821319 |
| ISENTROPIC | 0.66 | 1.126535 | 0.919862 | 1.4 | 0.746498 | 0.811533 |
| ISENTROPIC | 0.68 | 1.109655 | 0.915349 | 1.4 | 0.733758 | 0.801616 |
| ISENTROPIC | 0.7 | 1.094373 | 0.910747 | 1.4 | 0.720928 | 0.791579 |
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