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Compressible Flow: RAYLEIGH

0.72 to 0.9

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 5 of 15
flow typemach numberT0 T0star (dimensionless)T Tstar (dimensionless)V Vstar (dimensionless)gamma (dimensionless)p0 p0star (dimensionless)p pstar (dimensionless)
RAYLEIGH0.720.9221221.0025980.7209351.41.0376421.390692
RAYLEIGH0.740.9344231.0106240.7439211.41.0325281.358511
RAYLEIGH0.760.9454561.0170570.7664541.41.0277691.326964
RAYLEIGH0.780.9552791.021980.7885261.41.0233721.296064
RAYLEIGH0.80.9639481.0254770.8101271.41.0193431.265823
RAYLEIGH0.820.9715241.0276330.8312521.41.0156871.236247
RAYLEIGH0.840.9780661.0285330.85191.41.0124071.207341
RAYLEIGH0.860.9836331.028260.8720671.41.0095071.179106
RAYLEIGH0.880.9882831.0268940.8917551.41.0069891.151543
RAYLEIGH0.90.9920731.0245160.9109651.41.0048561.124649

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