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Compressible Flow: NORMAL SHOCK

4 to 4.9

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 6 of 10
flow typemach numberM2 (dimensionless)T2 T1 (dimensionless)gamma (dimensionless)p02 p01 (dimensionless)p2 p1 (dimensionless)rho2 rho1 (dimensionless)
NORMAL SHOCK40.4349594.0468751.40.13875618.54.571429
NORMAL SHOCK4.10.4323634.2047931.40.12755619.4454.624484
NORMAL SHOCK4.20.4299384.3665711.40.11733420.4133334.674912
NORMAL SHOCK4.30.4276694.5322111.40.10800221.4054.722861
NORMAL SHOCK4.40.4255454.7017151.40.09948122.424.768473
NORMAL SHOCK4.50.4235524.8750861.40.09169823.4583334.811881
NORMAL SHOCK4.60.421685.0523251.40.08458624.524.853211
NORMAL SHOCK4.70.419925.2334351.40.07808625.6054.89258
NORMAL SHOCK4.80.4182635.4184161.40.0721426.7133334.9301
NORMAL SHOCK4.90.4167015.6072711.40.06669927.8454.965874

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