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Compressible Flow: RAYLEIGH

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: RAYLEIGH10 rowsPage 8 of 15
flow typemach numberT0 T0star (dimensionless)T Tstar (dimensionless)V Vstar (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
RAYLEIGH1.80.8362790.6089411.4046241.41.3159250.433526
RAYLEIGH1.850.8250370.5877381.4182851.41.3581080.4144
RAYLEIGH1.90.8141360.5673421.431121.41.40330.396432
RAYLEIGH1.950.8035840.5477431.4431881.41.4515950.379537
RAYLEIGH20.7933880.5289261.4545451.41.5030960.363636
RAYLEIGH2.050.7835490.5108711.4652431.41.5579120.34866
RAYLEIGH2.10.7740640.4935581.4753281.41.6161590.334541
RAYLEIGH2.150.7649280.4769621.4848421.41.6779610.321221
RAYLEIGH2.20.7561350.4610581.4938271.41.7434460.308642
RAYLEIGH2.250.7476760.4458191.5023181.41.8127510.296754

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