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Compressible Flow: FANNO

2.8 to 3.5

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.

Mechanical Engineeringflow type: FANNO10 rowsPage 10 of 15
flow typemach numberT Tstar (dimensionless)V Vstar (dimensionless)fLstar D (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
FANNO2.80.467291.9140410.4897651.43.5001230.244138
FANNO2.850.457231.9271350.4982841.43.6707190.237259
FANNO2.90.4474271.939810.5065161.43.8497680.230655
FANNO2.950.4378761.9520810.5144711.44.0376030.224313
FANNO30.4285711.9639610.5221591.44.2345680.218218
FANNO3.10.4106781.9866080.5367771.44.6573110.206723
FANNO3.20.3937012.0078590.5504441.45.1209580.19608
FANNO3.30.3775962.0278120.5632321.45.6286470.186209
FANNO3.40.3623192.046560.5752071.46.1836990.177038
FANNO3.50.3478262.0641870.5864291.46.7896210.168505

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