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Compressible Flow: FANNO
0.52 to 0.7
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 | 0.52 | 1.138434 | 0.554826 | 0.917418 | 1.4 | 1.303388 | 2.051873 |
| FANNO | 0.54 | 1.133873 | 0.575011 | 0.786625 | 1.4 | 1.270321 | 1.971916 |
| FANNO | 0.56 | 1.129178 | 0.595072 | 0.673571 | 1.4 | 1.240294 | 1.89755 |
| FANNO | 0.58 | 1.124353 | 0.615006 | 0.575683 | 1.4 | 1.213007 | 1.828199 |
| FANNO | 0.6 | 1.119403 | 0.634811 | 0.490822 | 1.4 | 1.1882 | 1.763364 |
| FANNO | 0.62 | 1.11433 | 0.654483 | 0.417197 | 1.4 | 1.165646 | 1.70261 |
| FANNO | 0.64 | 1.109139 | 0.67402 | 0.353299 | 1.4 | 1.145148 | 1.645558 |
| FANNO | 0.66 | 1.103834 | 0.693419 | 0.297853 | 1.4 | 1.126535 | 1.591871 |
| FANNO | 0.68 | 1.098418 | 0.712677 | 0.249775 | 1.4 | 1.109655 | 1.541257 |
| FANNO | 0.7 | 1.092896 | 0.731792 | 0.208139 | 1.4 | 1.094373 | 1.493452 |
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