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2.3 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 2.3 · T2 T1 1.9468 dimensionless · rho2 rho1 3.08455 dimensionless · p2 p1 6.005 dimensionless · M2 0.534411 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 2.3
M2 (dimensionless): 0.534411
T2 T1 (dimensionless): 1.946801
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.583295
P2 P1 (dimensionless): 6.005
RHO2 RHO1 (dimensionless): 3.084548

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