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1.9 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 1.9 · T2 T1 1.60792 dimensionless · rho2 rho1 2.51568 dimensionless · p2 p1 4.045 dimensionless · M2 0.595616 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 1.9
M2 (dimensionless): 0.595616
T2 T1 (dimensionless): 1.607916
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.767357
P2 P1 (dimensionless): 4.045
RHO2 RHO1 (dimensionless): 2.515679

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