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8.5 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 8.5 · T2 T1 14.9911 dimensionless · rho2 rho1 5.61165 dimensionless · p2 p1 84.125 dimensionless · M2 0.391211 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 8.5
M2 (dimensionless): 0.391211
T2 T1 (dimensionless): 14.991133
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.006449
P2 P1 (dimensionless): 84.125
RHO2 RHO1 (dimensionless): 5.61165

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