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Compressible Flow: RAYLEIGH

2.8 to 3.5

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 10 of 15
flow typemach numberT0 T0star (dimensionless)T Tstar (dimensionless)V Vstar (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
RAYLEIGH2.80.6737960.3148581.5711421.42.873080.200401
RAYLEIGH2.850.6685480.305681.5757181.43.0013560.193994
RAYLEIGH2.90.6635020.2968691.5800851.43.1358530.187882
RAYLEIGH2.950.6586480.2884071.5842531.43.2768040.182046
RAYLEIGH30.6539790.2802771.5882351.43.4244520.176471
RAYLEIGH3.10.6451620.2649541.5956831.43.7408440.166044
RAYLEIGH3.20.6369890.2507831.6025041.44.0871180.156495
RAYLEIGH3.30.6294050.2376611.6087651.44.4654890.147729
RAYLEIGH3.40.6223590.2254921.6145251.44.8783030.139665
RAYLEIGH3.50.6158050.2141931.6198351.45.3280350.132231

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