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Compressible Flow: NORMAL SHOCK
20 to 38
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 | M2 (dimensionless) | T2 T1 (dimensionless) | gamma (dimensionless) | p02 p01 (dimensionless) | p2 p1 (dimensionless) | po2 p1 (dimensionless) | rho2 rho1 (dimensionless) |
|---|---|---|---|---|---|---|---|---|
| NORMAL SHOCK | 20 | 0.3804 | 78.72 | 1.4 | 0.0001 | 466.5 | 515.5 | 5.926 |
| NORMAL SHOCK | 22 | 0.38 | 95.06 | 1.4 | 0.0001 | 564.5 | 623.6 | 5.939 |
| NORMAL SHOCK | 24 | 0.3796 | 112.9 | 1.4 | 0 | 671.8 | 742.1 | 5.948 |
| NORMAL SHOCK | 26 | 0.3794 | 132.4 | 1.4 | 0 | 788.5 | 870.9 | 5.956 |
| NORMAL SHOCK | 28 | 0.3792 | 153.4 | 1.4 | 0 | 914.5 | 1,010 | 5.962 |
| NORMAL SHOCK | 30 | 0.379 | 175.9 | 1.4 | 0 | 1,050 | 1,159 | 5.967 |
| NORMAL SHOCK | 32 | 0.3789 | 200.1 | 1.4 | 0 | 1,194 | 1,319 | 5.971 |
| NORMAL SHOCK | 34 | 0.3788 | 225.7 | 1.4 | 0 | 1,348 | 1,489 | 5.974 |
| NORMAL SHOCK | 36 | 0.3787 | 252.9 | 1.4 | 0 | 1,512 | 1,669 | 5.977 |
| NORMAL SHOCK | 38 | 0.3786 | 281.7 | 1.4 | 0 | 1,684 | 1,860 | 5.979 |
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