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Compressible Flow: ISENTROPIC
0.32 to 0.5
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 | 0.32 | 1.921851 | 0.979931 | 1.4 | 0.931503 | 0.95058 |
| ISENTROPIC | 0.34 | 1.822876 | 0.977402 | 1.4 | 0.923118 | 0.94446 |
| ISENTROPIC | 0.36 | 1.735778 | 0.974735 | 1.4 | 0.91433 | 0.938029 |
| ISENTROPIC | 0.38 | 1.658696 | 0.971931 | 1.4 | 0.905156 | 0.931297 |
| ISENTROPIC | 0.4 | 1.59014 | 0.968992 | 1.4 | 0.895614 | 0.924274 |
| ISENTROPIC | 0.42 | 1.528905 | 0.965922 | 1.4 | 0.885722 | 0.916971 |
| ISENTROPIC | 0.44 | 1.474005 | 0.962723 | 1.4 | 0.875498 | 0.909398 |
| ISENTROPIC | 0.46 | 1.424629 | 0.959398 | 1.4 | 0.86496 | 0.901566 |
| ISENTROPIC | 0.48 | 1.380097 | 0.95595 | 1.4 | 0.854128 | 0.893486 |
| ISENTROPIC | 0.5 | 1.339844 | 0.952381 | 1.4 | 0.843019 | 0.88517 |
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