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9.5 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 9.5 · T2 T1 18.4915 dimensionless · rho2 rho1 5.68504 dimensionless · p2 p1 105.125 dimensionless · M2 0.388601 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 9.5
M2 (dimensionless): 0.388601
T2 T1 (dimensionless): 18.491517
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.003866
P2 P1 (dimensionless): 105.125
RHO2 RHO1 (dimensionless): 5.685039

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