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4.9 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 4.9 · T2 T1 5.60727 dimensionless · rho2 rho1 4.96587 dimensionless · p2 p1 27.845 dimensionless · M2 0.416701 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 4.9
M2 (dimensionless): 0.416701
T2 T1 (dimensionless): 5.607271
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.066699
P2 P1 (dimensionless): 27.845
RHO2 RHO1 (dimensionless): 4.965874

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