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Compressible Flow: RAYLEIGH

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: RAYLEIGH10 rowsPage 9 of 15
flow typemach numberT0 T0star (dimensionless)T Tstar (dimensionless)V Vstar (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
RAYLEIGH2.30.7395430.431221.510351.41.886020.28551
RAYLEIGH2.350.7317250.4172351.5179521.41.9634020.274867
RAYLEIGH2.40.7242130.4038361.5251541.42.0450550.264784
RAYLEIGH2.450.7169940.3909991.5319831.42.1311410.255224
RAYLEIGH2.50.7100590.3786981.5384621.42.2218310.246154
RAYLEIGH2.550.7033960.366911.5446131.42.3173030.237541
RAYLEIGH2.60.6969950.355611.5504591.42.4177410.229358
RAYLEIGH2.650.6908450.3447761.5560171.42.5233360.221576
RAYLEIGH2.70.6849350.3343871.5613061.42.6342850.214171
RAYLEIGH2.750.6792560.3244211.5663431.42.7507960.20712

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