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Compressible Flow: RAYLEIGH

0.52 to 0.7

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 4 of 15
flow typemach numberT0 T0star (dimensionless)T Tstar (dimensionless)V Vstar (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
RAYLEIGH0.520.7198970.8195540.4707521.41.1058821.740947
RAYLEIGH0.540.7469520.8469480.4969611.41.0978921.704255
RAYLEIGH0.560.7724860.8722740.5230151.41.0901091.667779
RAYLEIGH0.580.7964780.8955230.5488661.41.0825561.631588
RAYLEIGH0.60.8189230.9167040.5744681.41.0752531.595745
RAYLEIGH0.620.8398250.9358430.5997821.41.0682211.560306
RAYLEIGH0.640.8592030.9529760.6247711.41.0614751.52532
RAYLEIGH0.660.8770840.9681550.6494061.41.0550311.490831
RAYLEIGH0.680.8935020.9814390.673661.41.0489041.456876
RAYLEIGH0.70.9084990.9928950.6975091.41.0431041.423488

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