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3.2 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 3.2 · T2 T1 2.92199 dimensionless · rho2 rho1 4.0315 dimensionless · p2 p1 11.78 dimensionless · M2 0.464349 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 3.2
M2 (dimensionless): 0.464349
T2 T1 (dimensionless): 2.921992
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.276229
P2 P1 (dimensionless): 11.78
RHO2 RHO1 (dimensionless): 4.031496

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