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Compressible Flow: PRANDTL MEYER

1.6 to 1.78

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 4 of 17
flow typemach numbergamma (dimensionless)mu deg (degrees)nu deg (degrees)
PRANDTL MEYER1.61.438.6814.86
PRANDTL MEYER1.621.438.1215.45
PRANDTL MEYER1.641.437.5716.04
PRANDTL MEYER1.661.437.0416.63
PRANDTL MEYER1.681.436.5317.22
PRANDTL MEYER1.71.436.0317.81
PRANDTL MEYER1.721.435.5518.4
PRANDTL MEYER1.741.435.0818.98
PRANDTL MEYER1.761.434.6219.56
PRANDTL MEYER1.781.434.1820.15

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