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Compressible Flow: RAYLEIGH
0.92 to 1.25
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.
| flow type | mach number | T0 T0star (dimensionless) | T Tstar (dimensionless) | V Vstar (dimensionless) | gamma (dimensionless) | p0 p0star (dimensionless) | p pstar (dimensionless) |
|---|---|---|---|---|---|---|---|
| RAYLEIGH | 0.92 | 0.995058 | 1.021201 | 0.929701 | 1.4 | 1.003109 | 1.098418 |
| RAYLEIGH | 0.94 | 0.997293 | 1.017023 | 0.947967 | 1.4 | 1.001749 | 1.072846 |
| RAYLEIGH | 0.96 | 0.998828 | 1.012052 | 0.965768 | 1.4 | 1.000778 | 1.047925 |
| RAYLEIGH | 0.98 | 0.999715 | 1.006357 | 0.98311 | 1.4 | 1.000194 | 1.023646 |
| RAYLEIGH | 1 | 1 | 1 | 1 | 1.4 | 1 | 1 |
| RAYLEIGH | 1.05 | 0.998376 | 0.981607 | 1.040299 | 1.4 | 1.001215 | 0.943582 |
| RAYLEIGH | 1.1 | 0.993924 | 0.960313 | 1.077951 | 1.4 | 1.004858 | 0.890869 |
| RAYLEIGH | 1.15 | 0.987209 | 0.936853 | 1.113098 | 1.4 | 1.010926 | 0.841662 |
| RAYLEIGH | 1.2 | 0.978717 | 0.911848 | 1.145889 | 1.4 | 1.019415 | 0.795756 |
| RAYLEIGH | 1.25 | 0.968858 | 0.885813 | 1.176471 | 1.4 | 1.030325 | 0.752941 |
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