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Compressible Flow: NORMAL SHOCK

5 to 9.5

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 7 of 10
flow typemach numberM2 (dimensionless)T2 T1 (dimensionless)gamma (dimensionless)p02 p01 (dimensionless)p2 p1 (dimensionless)rho2 rho1 (dimensionless)
NORMAL SHOCK50.4152275.81.40.061716295
NORMAL SHOCK5.50.4089746.8217981.40.04236135.1255.148936
NORMAL SHOCK60.4041627.9405861.40.02965141.8333335.268293
NORMAL SHOCK6.50.4003819.1564351.40.02114849.1255.365079
NORMAL SHOCK70.3973610.4693881.40.015351575.444444
NORMAL SHOCK7.50.39490711.8794751.40.01132965.4583335.510204
NORMAL SHOCK80.3928913.3867191.40.00848874.55.565217
NORMAL SHOCK8.50.39121114.9911331.40.00644984.1255.61165
NORMAL SHOCK90.38979916.692731.40.00496494.3333335.651163
NORMAL SHOCK9.50.38860118.4915171.40.003866105.1255.685039

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