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Compressible Flow: FANNO

8 to 15

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 13 of 15
flow typemach numberT Tstar (dimensionless)V Vstar (dimensionless)fLstar D (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)rho rhostar (dimensionless)
FANNO80.0869572.3590710.7681921.4190.1093750.03686
FANNO8.50.077672.3688920.7740391.4251.0861670.032787
FANNO90.0697672.3772170.7789851.4327.18930.029348
FANNO9.50.0629922.3843320.7832041.4421.1313730.026419
FANNO100.0571432.3904570.7868311.4535.93750.023905
FANNO110.047620.79271.4841.90.019840.4166
FANNO120.040270.79721.41,2760.016720.4153
FANNO130.034480.80071.41,8760.014280.4142
FANNO140.029850.80361.42,6850.012340.4134
FANNO150.026090.80581.43,7550.010770.4128

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