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Compressible Flow: FANNO

0.72 to 0.9

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 5 of 15
flow typemach numberT Tstar (dimensionless)V Vstar (dimensionless)fLstar D (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
FANNO0.721.0872720.7507610.1721491.41.0805711.448227
FANNO0.741.0815490.7695820.1411221.41.0681441.405372
FANNO0.761.0757310.7882530.1144681.41.0569991.364704
FANNO0.781.0698240.8067720.0916721.41.0470531.326055
FANNO0.81.063830.8251370.072291.41.038231.289277
FANNO0.821.0577530.8433470.0559321.41.0304641.254233
FANNO0.841.0515980.8613990.0422561.41.0236961.220803
FANNO0.861.0453690.8792920.0309651.41.0178711.188875
FANNO0.881.0390690.8970260.0217951.41.0129411.158349
FANNO0.91.0327020.9145980.0145121.41.0088631.129133

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