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Compressible Flow: FANNO
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 | T Tstar (dimensionless) | V Vstar (dimensionless) | fLstar D (dimensionless) | gamma (dimensionless) | p0 p0star (dimensionless) | p pstar (dimensionless) |
|---|---|---|---|---|---|---|---|
| FANNO | 4.6 | 0.229358 | 2.203 | 0.673448 | 1.4 | 18.017795 | 0.104112 |
| FANNO | 4.7 | 0.221484 | 2.211918 | 0.678952 | 1.4 | 19.582828 | 0.100132 |
| FANNO | 4.8 | 0.21398 | 2.220383 | 0.684167 | 1.4 | 21.26371 | 0.096371 |
| FANNO | 4.9 | 0.206825 | 2.228424 | 0.689112 | 1.4 | 23.067119 | 0.092812 |
| FANNO | 5 | 0.2 | 2.236068 | 0.693804 | 1.4 | 25 | 0.089443 |
| FANNO | 5.5 | 0.170213 | 2.269127 | 0.714004 | 1.4 | 36.868963 | 0.075012 |
| FANNO | 6 | 0.146341 | 2.295276 | 0.729875 | 1.4 | 53.179784 | 0.063758 |
| FANNO | 6.5 | 0.126984 | 2.316264 | 0.742544 | 1.4 | 75.134315 | 0.054823 |
| FANNO | 7 | 0.111111 | 2.333333 | 0.752802 | 1.4 | 104.142857 | 0.047619 |
| FANNO | 7.5 | 0.097959 | 2.347382 | 0.761214 | 1.4 | 141.841483 | 0.041731 |
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