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Compressible Flow: ISENTROPIC
1.3 to 1.75
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 | A Astar (dimensionless) | T T0 (dimensionless) | gamma (dimensionless) | p p0 (dimensionless) | rho rho0 (dimensionless) |
|---|---|---|---|---|---|---|
| ISENTROPIC | 1.3 | 1.066305 | 0.747384 | 1.4 | 0.360914 | 0.482903 |
| ISENTROPIC | 1.35 | 1.089038 | 0.732869 | 1.4 | 0.336971 | 0.459797 |
| ISENTROPIC | 1.4 | 1.114926 | 0.718391 | 1.4 | 0.314241 | 0.437423 |
| ISENTROPIC | 1.45 | 1.143963 | 0.703977 | 1.4 | 0.292722 | 0.415812 |
| ISENTROPIC | 1.5 | 1.176167 | 0.689655 | 1.4 | 0.272403 | 0.394984 |
| ISENTROPIC | 1.55 | 1.211574 | 0.675447 | 1.4 | 0.253262 | 0.374955 |
| ISENTROPIC | 1.6 | 1.250235 | 0.661376 | 1.4 | 0.235271 | 0.35573 |
| ISENTROPIC | 1.65 | 1.292219 | 0.647459 | 1.4 | 0.218395 | 0.337311 |
| ISENTROPIC | 1.7 | 1.337606 | 0.633714 | 1.4 | 0.202593 | 0.319693 |
| ISENTROPIC | 1.75 | 1.386492 | 0.620155 | 1.4 | 0.187824 | 0.302866 |
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