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Compressible Flow: FANNO

1.3 to 1.75

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.

Mechanical Engineeringflow type: FANNO10 rowsPage 7 of 15
flow typemach numberT Tstar (dimensionless)V Vstar (dimensionless)fLstar D (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
FANNO1.30.8968611.2311360.0648321.41.0663050.728483
FANNO1.350.8794431.2660110.0819911.41.0890380.694656
FANNO1.40.8620691.2998670.0997381.41.1149260.663198
FANNO1.450.8447731.3327170.1178231.41.1439630.633873
FANNO1.50.8275861.3645760.136051.41.1761670.606478
FANNO1.550.8105371.3954620.1542681.41.2115740.580838
FANNO1.60.7936511.4253930.1723571.41.2502350.556794
FANNO1.650.776951.4543890.1902261.41.2922190.534211
FANNO1.70.7604561.482470.2078031.41.3376060.512966
FANNO1.750.7441861.5096590.2250371.41.3864920.49295

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