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Compressible Flow: NORMAL SHOCK
10 to 19
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 | 11 | 0.3859 | 24.47 | 1.4 | 0.0019 | 141 | 156.3 | 5.762 |
| NORMAL SHOCK | 12 | 0.3847 | 28.94 | 1.4 | 0.0013 | 167.8 | 185.9 | 5.799 |
| NORMAL SHOCK | 13 | 0.3837 | 33.8 | 1.4 | 0.0009 | 197 | 218.1 | 5.828 |
| NORMAL SHOCK | 14 | 0.3829 | 39.05 | 1.4 | 0.0006 | 228.5 | 252.8 | 5.851 |
| NORMAL SHOCK | 15 | 0.3823 | 44.69 | 1.4 | 0.0004 | 262.3 | 290.2 | 5.87 |
| NORMAL SHOCK | 16 | 0.3817 | 50.72 | 1.4 | 0.0003 | 298.5 | 330.1 | 5.885 |
| NORMAL SHOCK | 17 | 0.3813 | 57.14 | 1.4 | 0.0002 | 337 | 372.6 | 5.898 |
| NORMAL SHOCK | 18 | 0.381 | 63.94 | 1.4 | 0.0002 | 377.8 | 417.6 | 5.909 |
| NORMAL SHOCK | 19 | 0.3806 | 71.14 | 1.4 | 0.0001 | 421 | 465.3 | 5.918 |
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