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Compressible Flow: FANNO
0.32 to 0.5
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 | 0.32 | 1.175917 | 0.347007 | 4.446743 | 1.4 | 1.921851 | 3.388741 |
| FANNO | 0.34 | 1.172883 | 0.368219 | 3.751953 | 1.4 | 1.822876 | 3.185286 |
| FANNO | 0.36 | 1.169682 | 0.389347 | 3.180118 | 1.4 | 1.735778 | 3.004218 |
| FANNO | 0.38 | 1.166317 | 0.410385 | 2.705448 | 1.4 | 1.658696 | 2.842004 |
| FANNO | 0.4 | 1.162791 | 0.431331 | 2.308493 | 1.4 | 1.59014 | 2.695819 |
| FANNO | 0.42 | 1.159107 | 0.45218 | 1.974366 | 1.4 | 1.528905 | 2.563377 |
| FANNO | 0.44 | 1.155268 | 0.472927 | 1.691525 | 1.4 | 1.474005 | 2.442804 |
| FANNO | 0.46 | 1.151278 | 0.493569 | 1.450911 | 1.4 | 1.424629 | 2.332557 |
| FANNO | 0.48 | 1.14714 | 0.514102 | 1.245341 | 1.4 | 1.380097 | 2.231346 |
| FANNO | 0.5 | 1.142857 | 0.534522 | 1.06906 | 1.4 | 1.339844 | 2.13809 |
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