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Compressible Flow: PRANDTL MEYER

1.2 to 1.38

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: PRANDTL MEYER10 rowsPage 2 of 17
flow typemach numbergamma (dimensionless)mu deg (degrees)nu deg (degrees)
PRANDTL MEYER1.21.456.443.558
PRANDTL MEYER1.221.455.054.057
PRANDTL MEYER1.241.453.754.569
PRANDTL MEYER1.261.452.535.093
PRANDTL MEYER1.281.451.385.627
PRANDTL MEYER1.31.450.286.17
PRANDTL MEYER1.321.449.256.721
PRANDTL MEYER1.341.448.277.279
PRANDTL MEYER1.361.447.337.844
PRANDTL MEYER1.381.446.448.413

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