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Compressible Flow: FANNO
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 | T Tstar (dimensionless) | V Vstar (dimensionless) | fLstar D (dimensionless) | gamma (dimensionless) | p0 p0star (dimensionless) | p pstar (dimensionless) |
|---|---|---|---|---|---|---|---|
| FANNO | 0.12 | 1.196554 | 0.131265 | 45.407962 | 1.4 | 4.864318 | 9.115592 |
| FANNO | 0.14 | 1.195314 | 0.153063 | 32.511306 | 1.4 | 4.1824 | 7.809317 |
| FANNO | 0.16 | 1.193887 | 0.174824 | 24.19783 | 1.4 | 3.672739 | 6.829072 |
| FANNO | 0.18 | 1.192274 | 0.196544 | 18.542654 | 1.4 | 3.277926 | 6.066183 |
| FANNO | 0.2 | 1.190476 | 0.218218 | 14.533266 | 1.4 | 2.96352 | 5.455447 |
| FANNO | 0.22 | 1.188495 | 0.23984 | 11.596054 | 1.4 | 2.707602 | 4.95537 |
| FANNO | 0.24 | 1.186333 | 0.261405 | 9.386481 | 1.4 | 2.495562 | 4.538289 |
| FANNO | 0.26 | 1.183992 | 0.28291 | 7.687567 | 1.4 | 2.317287 | 4.185054 |
| FANNO | 0.28 | 1.181474 | 0.304348 | 6.357214 | 1.4 | 2.165554 | 3.881988 |
| FANNO | 0.3 | 1.178782 | 0.325715 | 5.299253 | 1.4 | 2.035065 | 3.619057 |
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