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1.65 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 1.65 · T2 T1 1.4228 dimensionless · rho2 rho1 2.11525 dimensionless · p2 p1 3.00958 dimensionless · M2 0.653958 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 1.65
M2 (dimensionless): 0.653958
T2 T1 (dimensionless): 1.422804
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.875988
P2 P1 (dimensionless): 3.009583
RHO2 RHO1 (dimensionless): 2.115248

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