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Compressible Flow: ISENTROPIC
1.8 to 2.25
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 | 1.8 | 1.438982 | 0.606796 | 1.4 | 0.17404 | 0.286818 |
| ISENTROPIC | 1.85 | 1.495194 | 0.593648 | 1.4 | 0.161195 | 0.271533 |
| ISENTROPIC | 1.9 | 1.555257 | 0.58072 | 1.4 | 0.14924 | 0.256991 |
| ISENTROPIC | 1.95 | 1.619309 | 0.56802 | 1.4 | 0.138126 | 0.24317 |
| ISENTROPIC | 2 | 1.6875 | 0.555556 | 1.4 | 0.127805 | 0.230048 |
| ISENTROPIC | 2.05 | 1.759989 | 0.543331 | 1.4 | 0.118229 | 0.217601 |
| ISENTROPIC | 2.1 | 1.836944 | 0.53135 | 1.4 | 0.109353 | 0.205803 |
| ISENTROPIC | 2.15 | 1.918543 | 0.519615 | 1.4 | 0.101132 | 0.194628 |
| ISENTROPIC | 2.2 | 2.004975 | 0.50813 | 1.4 | 0.093522 | 0.184051 |
| ISENTROPIC | 2.25 | 2.096435 | 0.496894 | 1.4 | 0.086482 | 0.174044 |
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