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Compressible Flow: FANNO
3.6 to 4.5
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 | 3.6 | 0.334076 | 2.080774 | 0.596955 | 1.4 | 7.450111 | 0.160554 |
| FANNO | 3.7 | 0.321027 | 2.096393 | 0.606836 | 1.4 | 8.169066 | 0.153133 |
| FANNO | 3.8 | 0.308642 | 2.111111 | 0.616119 | 1.4 | 8.950585 | 0.146199 |
| FANNO | 3.9 | 0.296883 | 2.124991 | 0.624849 | 1.4 | 9.798973 | 0.13971 |
| FANNO | 4 | 0.285714 | 2.13809 | 0.633065 | 1.4 | 10.71875 | 0.133631 |
| FANNO | 4.1 | 0.275103 | 2.150461 | 0.640804 | 1.4 | 11.714652 | 0.127928 |
| FANNO | 4.2 | 0.265018 | 2.162154 | 0.648101 | 1.4 | 12.79164 | 0.122571 |
| FANNO | 4.3 | 0.255428 | 2.173214 | 0.654986 | 1.4 | 13.954904 | 0.117535 |
| FANNO | 4.4 | 0.246305 | 2.183683 | 0.661489 | 1.4 | 15.209867 | 0.112794 |
| FANNO | 4.5 | 0.237624 | 2.1936 | 0.667635 | 1.4 | 16.562195 | 0.108326 |
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