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Compressible Flow: NORMAL SHOCK

2 to 2.45

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.

Mechanical Engineeringflow type: NORMAL SHOCK10 rowsPage 3 of 10
flow typemach numberM2 (dimensionless)T2 T1 (dimensionless)gamma (dimensionless)p02 p01 (dimensionless)p2 p1 (dimensionless)rho2 rho1 (dimensionless)
NORMAL SHOCK20.577351.68751.40.7208744.52.666667
NORMAL SHOCK2.050.5690631.7285481.40.6975084.736252.740016
NORMAL SHOCK2.10.5612771.770451.40.6742034.9783332.811902
NORMAL SHOCK2.150.5539531.8132181.40.6510525.226252.882307
NORMAL SHOCK2.20.5470561.856861.40.6281365.482.95122
NORMAL SHOCK2.250.5405521.9013851.40.605535.7395833.018634
NORMAL SHOCK2.30.5344111.9468011.40.5832956.0053.084548
NORMAL SHOCK2.350.5286081.9931141.40.5614846.276253.148967
NORMAL SHOCK2.40.5231182.0403321.40.5401446.5533333.211896
NORMAL SHOCK2.450.5179182.0884591.40.5193116.836253.273347

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