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Compressible Flow: RAYLEIGH

0.12 to 0.3

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 2 of 15
flow typemach numberT0 T0star (dimensionless)T Tstar (dimensionless)V Vstar (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
RAYLEIGH0.120.0666060.0796980.0338771.41.2553942.352572
RAYLEIGH0.140.0894710.1069460.0457841.41.2510292.335903
RAYLEIGH0.160.115110.1374290.0593141.41.2460832.31696
RAYLEIGH0.180.1432380.1707790.0743861.41.2405922.29586
RAYLEIGH0.20.1735540.2066120.0909091.41.2345962.272727
RAYLEIGH0.220.2057420.2445230.1087881.41.2281362.247696
RAYLEIGH0.240.2394840.2841080.1279241.41.2212552.220906
RAYLEIGH0.260.2744590.3249570.1482131.41.2142.192502
RAYLEIGH0.280.3103530.3666740.169551.41.2064162.16263
RAYLEIGH0.30.346860.4088730.1918291.41.1985492.131439

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