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Compressible Flow: ISENTROPIC
4.6 to 7.5
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 | 4.6 | 18.017795 | 0.191131 | 1.4 | 0.003053 | 0.015971 |
| ISENTROPIC | 4.7 | 19.582828 | 0.18457 | 1.4 | 0.002701 | 0.014635 |
| ISENTROPIC | 4.8 | 21.26371 | 0.178317 | 1.4 | 0.002394 | 0.013427 |
| ISENTROPIC | 4.9 | 23.067119 | 0.172354 | 1.4 | 0.002126 | 0.012333 |
| ISENTROPIC | 5 | 25 | 0.166667 | 1.4 | 0.00189 | 0.01134 |
| ISENTROPIC | 5.5 | 36.868963 | 0.141844 | 1.4 | 0.001075 | 0.007578 |
| ISENTROPIC | 6 | 53.179784 | 0.121951 | 1.4 | 0.000633 | 0.005194 |
| ISENTROPIC | 6.5 | 75.134315 | 0.10582 | 1.4 | 0.000385 | 0.003643 |
| ISENTROPIC | 7 | 104.142857 | 0.092593 | 1.4 | 0.000242 | 0.002609 |
| ISENTROPIC | 7.5 | 141.841483 | 0.081633 | 1.4 | 0.000155 | 0.001904 |
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