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Compressible Flow: RAYLEIGH
8 to 15
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) | rho rhostar (dimensionless) |
|---|---|---|---|---|---|---|---|---|
| RAYLEIGH | 8 | 0.516469 | 0.04491 | 1.695364 | 1.4 | 136.623525 | 0.02649 | — |
| RAYLEIGH | 8.5 | 0.513489 | 0.039883 | 1.697504 | 1.4 | 179.923629 | 0.023495 | — |
| RAYLEIGH | 9 | 0.510979 | 0.03565 | 1.699301 | 1.4 | 233.88395 | 0.020979 | — |
| RAYLEIGH | 9.5 | 0.508845 | 0.032053 | 1.700824 | 1.4 | 300.407217 | 0.018846 | — |
| RAYLEIGH | 10 | 0.507017 | 0.028972 | 1.702128 | 1.4 | 381.614879 | 0.017021 | — |
| RAYLEIGH | 11 | 0.5041 | 0.024 | — | 1.4 | 597.7 | 0.01408 | 0.5868 |
| RAYLEIGH | 12 | 0.5018 | 0.02021 | — | 1.4 | 904.1 | 0.01185 | 0.5862 |
| RAYLEIGH | 13 | 0.5001 | 0.01724 | — | 1.4 | 1,327 | 0.0101 | 0.5858 |
| RAYLEIGH | 14 | 0.4986 | 0.01489 | — | 1.4 | 1,896 | 0.008715 | 0.5855 |
| RAYLEIGH | 15 | 0.4975 | 0.01298 | — | 1.4 | 2,649 | 0.007595 | 0.5852 |
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