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Compressible Flow: NORMAL SHOCK

20 to 38

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 9 of 10
flow typemach numberM2 (dimensionless)T2 T1 (dimensionless)gamma (dimensionless)p02 p01 (dimensionless)p2 p1 (dimensionless)po2 p1 (dimensionless)rho2 rho1 (dimensionless)
NORMAL SHOCK200.380478.721.40.0001466.5515.55.926
NORMAL SHOCK220.3895.061.40.0001564.5623.65.939
NORMAL SHOCK240.3796112.91.40671.8742.15.948
NORMAL SHOCK260.3794132.41.40788.5870.95.956
NORMAL SHOCK280.3792153.41.40914.51,0105.962
NORMAL SHOCK300.379175.91.401,0501,1595.967
NORMAL SHOCK320.3789200.11.401,1941,3195.971
NORMAL SHOCK340.3788225.71.401,3481,4895.974
NORMAL SHOCK360.3787252.91.401,5121,6695.977
NORMAL SHOCK380.3786281.71.401,6841,8605.979

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