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Compressible Flow: ISENTROPIC
0.12 to 0.3
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 | 0.12 | 4.864318 | 0.997128 | 1.4 | 0.989985 | 0.992836 |
| ISENTROPIC | 0.14 | 4.1824 | 0.996095 | 1.4 | 0.9864 | 0.990267 |
| ISENTROPIC | 0.16 | 3.672739 | 0.994906 | 1.4 | 0.982285 | 0.987314 |
| ISENTROPIC | 0.18 | 3.277926 | 0.993562 | 1.4 | 0.977647 | 0.983982 |
| ISENTROPIC | 0.2 | 2.96352 | 0.992063 | 1.4 | 0.972497 | 0.980277 |
| ISENTROPIC | 0.22 | 2.707602 | 0.990413 | 1.4 | 0.966845 | 0.976204 |
| ISENTROPIC | 0.24 | 2.495562 | 0.988611 | 1.4 | 0.960703 | 0.971771 |
| ISENTROPIC | 0.26 | 2.317287 | 0.98666 | 1.4 | 0.954085 | 0.966984 |
| ISENTROPIC | 0.28 | 2.165554 | 0.984562 | 1.4 | 0.947002 | 0.961851 |
| ISENTROPIC | 0.3 | 2.035065 | 0.982318 | 1.4 | 0.93947 | 0.95638 |
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