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Compressible Flow: NORMAL SHOCK
1.5 to 1.95
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) | rho2 rho1 (dimensionless) |
|---|---|---|---|---|---|---|---|
| NORMAL SHOCK | 1.5 | 0.701089 | 1.320216 | 1.4 | 0.929787 | 2.458333 | 1.862069 |
| NORMAL SHOCK | 1.55 | 0.684101 | 1.353787 | 1.4 | 0.913188 | 2.63625 | 1.947315 |
| NORMAL SHOCK | 1.6 | 0.668437 | 1.387969 | 1.4 | 0.8952 | 2.82 | 2.031746 |
| NORMAL SHOCK | 1.65 | 0.653958 | 1.422804 | 1.4 | 0.875988 | 3.009583 | 2.115248 |
| NORMAL SHOCK | 1.7 | 0.640544 | 1.45833 | 1.4 | 0.855721 | 3.205 | 2.197719 |
| NORMAL SHOCK | 1.75 | 0.628089 | 1.494579 | 1.4 | 0.834565 | 3.40625 | 2.27907 |
| NORMAL SHOCK | 1.8 | 0.616501 | 1.531578 | 1.4 | 0.812684 | 3.613333 | 2.359223 |
| NORMAL SHOCK | 1.85 | 0.605701 | 1.569349 | 1.4 | 0.790232 | 3.82625 | 2.438112 |
| NORMAL SHOCK | 1.9 | 0.595616 | 1.607916 | 1.4 | 0.767357 | 4.045 | 2.515679 |
| NORMAL SHOCK | 1.95 | 0.586185 | 1.647294 | 1.4 | 0.744195 | 4.269583 | 2.591877 |
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