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2.5 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 2.5 · T2 T1 2.1375 dimensionless · rho2 rho1 3.33333 dimensionless · p2 p1 7.125 dimensionless · M2 0.512989 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 2.5
M2 (dimensionless): 0.512989
T2 T1 (dimensionless): 2.1375
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.499015
P2 P1 (dimensionless): 7.125
RHO2 RHO1 (dimensionless): 3.333333

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