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Compressible Flow: FANNO
16 to 30
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) | fLstar D (dimensionless) | gamma (dimensionless) | p0 p0star (dimensionless) | p pstar (dimensionless) | rho rhostar (dimensionless) |
|---|---|---|---|---|---|---|---|
| FANNO | 16 | 0.02299 | 0.8077 | 1.4 | 5,145 | 0.009476 | 0.4122 |
| FANNO | 17 | 0.02041 | 0.8093 | 1.4 | 6,921 | 0.008403 | 0.4118 |
| FANNO | 18 | 0.01824 | 0.8106 | 1.4 | 9,159 | 0.007502 | 0.4114 |
| FANNO | 19 | 0.01639 | 0.8117 | 1.4 | 11,950 | 0.006739 | 0.4111 |
| FANNO | 20 | 0.01481 | 0.8126 | 1.4 | 15,380 | 0.006086 | 0.4108 |
| FANNO | 22 | 0.01227 | 0.8142 | 1.4 | 24,610 | 0.005035 | 0.4104 |
| FANNO | 24 | 0.01033 | 0.8153 | 1.4 | 37,830 | 0.004234 | 0.41 |
| FANNO | 26 | 0.008811 | 0.8162 | 1.4 | 56,240 | 0.00361 | 0.4098 |
| FANNO | 28 | 0.007605 | 0.817 | 1.4 | 81,210 | 0.003114 | 0.4095 |
| FANNO | 30 | 0.00663 | 0.8176 | 1.4 | 114,400 | 0.002714 | 0.4094 |
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