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Compressible Flow: FANNO

0.92 to 1.25

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 6 of 15
flow typemach numberT Tstar (dimensionless)V Vstar (dimensionless)fLstar D (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
FANNO0.921.0262730.9320070.0089131.41.0055971.101143
FANNO0.941.0197840.9492530.0048151.41.0031081.074302
FANNO0.961.013240.9663340.0020571.41.0013651.04854
FANNO0.981.0066440.983250.0004951.41.0003371.023792
FANNO11101.411
FANNO1.050.9832041.0411450.0027141.41.0020290.944349
FANNO1.10.9661841.0812410.0099351.41.0079250.893588
FANNO1.150.9489921.1202860.0205331.41.0174540.847097
FANNO1.20.9316771.1582810.0336381.41.030440.804362
FANNO1.250.9142861.1952290.0485791.41.0467530.764946

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