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Compressible Flow: FANNO

2.3 to 2.75

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 9 of 15
flow typemach numberT Tstar (dimensionless)V Vstar (dimensionless)fLstar D (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
FANNO2.30.583091.7562880.386231.42.1931310.332002
FANNO2.350.5702071.7745330.3982621.42.2952770.321328
FANNO2.40.5576211.7921760.4098891.42.40310.311142
FANNO2.450.5453311.8092390.4211231.42.5168320.301414
FANNO2.50.5333331.8257420.4319771.42.6367190.292119
FANNO2.550.5216261.8417030.4424611.42.7630120.28323
FANNO2.60.5102041.8571430.4525881.42.8959750.274725
FANNO2.650.4990641.8720790.462371.43.0358810.266583
FANNO2.70.4882021.8865290.4718191.43.1830110.258783
FANNO2.750.4776121.9005110.4809471.43.3376580.251307

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