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Compressible Flow: RAYLEIGH

4.6 to 7.5

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 12 of 15
flow typemach numberT0 T0star (dimensionless)T Tstar (dimensionless)V Vstar (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
RAYLEIGH4.60.5666320.1299611.6583071.413.5628840.07837
RAYLEIGH4.70.5636210.1248331.660591.414.7017450.075174
RAYLEIGH4.80.5607790.1199951.6627381.415.9233660.072167
RAYLEIGH4.90.5580940.1154281.664761.417.2324540.069336
RAYLEIGH50.5555560.1111111.6666671.418.63390.066667
RAYLEIGH5.50.5447250.0927191.674741.427.2113250.055363
RAYLEIGH60.5363290.0784871.6809341.438.9459450.046693
RAYLEIGH6.50.5296980.0672631.6857861.454.6830310.0399
RAYLEIGH70.5243760.0582641.6896551.475.4137930.034483
RAYLEIGH7.50.5200420.0509431.692791.4102.2874850.030094

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