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Compressible Flow: RAYLEIGH
32 to 50
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) | gamma (dimensionless) | p0 p0star (dimensionless) | p pstar (dimensionless) | rho rhostar (dimensionless) |
|---|---|---|---|---|---|---|---|
| RAYLEIGH | 32 | 0.4915 | 0.002866 | 1.4 | 110,500 | 0.001673 | 0.5837 |
| RAYLEIGH | 34 | 0.4913 | 0.002539 | 1.4 | 149,400 | 0.001482 | 0.5837 |
| RAYLEIGH | 36 | 0.4911 | 0.002265 | 1.4 | 198,500 | 0.001322 | 0.5837 |
| RAYLEIGH | 38 | 0.491 | 0.002033 | 1.4 | 259,700 | 0.001187 | 0.5836 |
| RAYLEIGH | 40 | 0.4909 | 0.001835 | 1.4 | 335,300 | 0.001071 | 0.5836 |
| RAYLEIGH | 42 | 0.4908 | 0.001665 | 1.4 | 427,500 | 0.000971 | 0.5836 |
| RAYLEIGH | 44 | 0.4907 | 0.001517 | 1.4 | 539,000 | 0.000885 | 0.5835 |
| RAYLEIGH | 46 | 0.4906 | 0.001388 | 1.4 | 672,600 | 0.00081 | 0.5835 |
| RAYLEIGH | 48 | 0.4906 | 0.001275 | 1.4 | 831,600 | 0.000744 | 0.5835 |
| RAYLEIGH | 50 | 0.4905 | 0.001175 | 1.4 | 1,019,000 | 0.000686 | 0.5835 |
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