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Compressible Flow: RAYLEIGH

3.6 to 4.5

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 11 of 15
flow typemach numberT0 T0star (dimensionless)T Tstar (dimensionless)V Vstar (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
RAYLEIGH3.60.6097010.2036861.6247391.45.8172980.125366
RAYLEIGH3.70.604010.1939041.6292771.46.3488440.119012
RAYLEIGH3.80.5986980.1847831.6334841.46.9255660.113122
RAYLEIGH3.90.5937320.1762691.6373911.47.5505040.107652
RAYLEIGH40.5890860.168311.6410261.48.2268490.102564
RAYLEIGH4.10.5847330.1608621.6444121.48.9579440.097823
RAYLEIGH4.20.5806510.1538831.6475721.49.7472890.0934
RAYLEIGH4.30.5768180.1473351.6505241.410.5985450.089266
RAYLEIGH4.40.5732150.1411861.6532881.411.5155380.085397
RAYLEIGH4.50.5698250.1354041.6558771.412.5022620.081772

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