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Compressible Flow: ISENTROPIC

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: ISENTROPIC10 rowsPage 5 of 15
flow typemach numberA Astar (dimensionless)T T0 (dimensionless)gamma (dimensionless)p p0 (dimensionless)rho rho0 (dimensionless)
ISENTROPIC0.721.0805710.906061.40.7080250.781434
ISENTROPIC0.741.0681440.9012911.40.6950680.771191
ISENTROPIC0.761.0569990.8964431.40.682070.760863
ISENTROPIC0.781.0470530.891521.40.669050.75046
ISENTROPIC0.81.038230.8865251.40.6560220.739992
ISENTROPIC0.821.0304640.8814611.40.6430.729471
ISENTROPIC0.841.0236960.8763321.40.630.718905
ISENTROPIC0.861.0178710.8711411.40.6170340.708306
ISENTROPIC0.881.0129410.8658911.40.6041170.697683
ISENTROPIC0.91.0088630.8605851.40.591260.687044

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