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Compressible Flow: NORMAL SHOCK

2.5 to 2.95

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 4 of 10
flow typemach numberM2 (dimensionless)T2 T1 (dimensionless)gamma (dimensionless)p02 p01 (dimensionless)p2 p1 (dimensionless)rho2 rho1 (dimensionless)
NORMAL SHOCK2.50.5129892.13751.40.4990157.1253.333333
NORMAL SHOCK2.550.5083122.187461.40.479287.4195833.391871
NORMAL SHOCK2.60.5038712.2383431.40.4601237.723.44898
NORMAL SHOCK2.650.4996492.2901531.40.4415578.026253.504679
NORMAL SHOCK2.70.4956342.3428921.40.423598.3383333.558991
NORMAL SHOCK2.750.491812.3965651.40.4062268.656253.61194
NORMAL SHOCK2.80.4881672.4511731.40.3894648.983.663551
NORMAL SHOCK2.850.4846942.506721.40.3733029.3095833.71385
NORMAL SHOCK2.90.481382.5632071.40.3577339.6453.762864
NORMAL SHOCK2.950.4782152.6206381.40.342759.986253.810619

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