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Compressible Flow: RAYLEIGH

1.3 to 1.75

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: RAYLEIGH10 rowsPage 7 of 15
flow typemach numberT0 T0star (dimensionless)T Tstar (dimensionless)V Vstar (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
RAYLEIGH1.30.9579790.8591741.2049911.41.043660.713012
RAYLEIGH1.350.9463650.8322741.2315921.41.059430.675771
RAYLEIGH1.40.9342540.8053911.256411.41.0776520.641026
RAYLEIGH1.450.9218380.7787441.2795741.41.0983460.608596
RAYLEIGH1.50.9092760.7525041.3012051.41.1215450.578313
RAYLEIGH1.550.8966920.7268021.3214161.41.1472850.550017
RAYLEIGH1.60.8841860.7017351.3403141.41.1756110.52356
RAYLEIGH1.650.8718390.6773751.3579961.41.2065740.498805
RAYLEIGH1.70.8597090.6537711.3745541.41.2402350.475624
RAYLEIGH1.750.8478450.6309541.3900711.41.2766610.453901

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