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Compressible Flow: RAYLEIGH
16 to 30
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 | 16 | 0.4966 | 0.01142 | 1.4 | 3,625 | 0.006678 | 0.585 |
| RAYLEIGH | 17 | 0.4958 | 0.01012 | 1.4 | 4,873 | 0.005917 | 0.5848 |
| RAYLEIGH | 18 | 0.4952 | 0.00903 | 1.4 | 6,445 | 0.005279 | 0.5846 |
| RAYLEIGH | 19 | 0.4946 | 0.008109 | 1.4 | 8,402 | 0.004739 | 0.5845 |
| RAYLEIGH | 20 | 0.4942 | 0.007321 | 1.4 | 10,810 | 0.004278 | 0.5844 |
| RAYLEIGH | 22 | 0.4934 | 0.006054 | 1.4 | 17,280 | 0.003537 | 0.5842 |
| RAYLEIGH | 24 | 0.4928 | 0.005089 | 1.4 | 26,560 | 0.002973 | 0.5841 |
| RAYLEIGH | 26 | 0.4924 | 0.004338 | 1.4 | 39,460 | 0.002533 | 0.5839 |
| RAYLEIGH | 28 | 0.492 | 0.003742 | 1.4 | 56,970 | 0.002185 | 0.5839 |
| RAYLEIGH | 30 | 0.4917 | 0.00326 | 1.4 | 80,210 | 0.001903 | 0.5838 |
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