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Compressible Flow: FANNO

1.8 to 2.25

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 8 of 15
flow typemach numberT Tstar (dimensionless)V Vstar (dimensionless)fLstar D (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
FANNO1.80.7281551.5359760.2418861.41.4389820.474067
FANNO1.850.7123781.5614460.2583241.41.4951940.45623
FANNO1.90.6968641.5860890.2743281.41.5552570.43936
FANNO1.950.6816251.6099310.2898881.41.6193090.423387
FANNO20.6666671.6329930.3049971.41.68750.408248
FANNO2.050.6519971.6552990.319651.41.7599890.393884
FANNO2.10.637621.6768730.3338511.41.8369440.380243
FANNO2.150.6235391.6977360.3476021.41.9185430.367277
FANNO2.20.6097561.7179110.360911.42.0049750.35494
FANNO2.250.5962731.7374220.3737831.42.0964350.343194

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