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Compressible Flow: NORMAL SHOCK
40 to 50
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 | 40 | 0.3786 | 312.1 | 1.4 | 0 | 1,866 | 2,061 | 5.981 |
| NORMAL SHOCK | 42 | 0.3785 | 343.9 | 1.4 | 0 | 2,058 | 2,272 | 5.983 |
| NORMAL SHOCK | 44 | 0.3785 | 377.4 | 1.4 | 0 | 2,258 | 2,493 | 5.985 |
| NORMAL SHOCK | 46 | 0.3784 | 412.4 | 1.4 | 0 | 2,468 | 2,725 | 5.986 |
| NORMAL SHOCK | 48 | 0.3784 | 448.9 | 1.4 | 0 | 2,688 | 2,967 | 5.987 |
| NORMAL SHOCK | 50 | 0.3784 | 487.1 | 1.4 | 0 | 2,916 | 3,219 | 5.988 |
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