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Compressible Flow: RAYLEIGH

0.32 to 0.5

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 3 of 15
flow typemach numberT0 T0star (dimensionless)T Tstar (dimensionless)V Vstar (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
RAYLEIGH0.320.3836890.4511870.2149451.41.1904462.099076
RAYLEIGH0.340.4205650.4932730.2387941.41.1821532.065689
RAYLEIGH0.360.4572320.5348160.2632721.41.1737142.031419
RAYLEIGH0.380.4934560.5755260.2882811.41.1651751.996406
RAYLEIGH0.40.5290270.6151480.3137251.41.1565771.960784
RAYLEIGH0.420.5637580.6534560.3395141.41.147961.924681
RAYLEIGH0.440.5974850.6902550.3655591.41.1393641.888218
RAYLEIGH0.460.6300680.7253830.3917791.41.1308251.851509
RAYLEIGH0.480.661390.7587070.4180981.41.1223771.814662
RAYLEIGH0.50.6913580.7901230.4444441.41.1140531.777778

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