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3.6 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 3.6 · T2 T1 3.45373 dimensionless · rho2 rho1 4.32962 dimensionless · p2 p1 14.9533 dimensionless · M2 0.447413 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 3.6
M2 (dimensionless): 0.447413
T2 T1 (dimensionless): 3.453728
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.195312
P2 P1 (dimensionless): 14.953333
RHO2 RHO1 (dimensionless): 4.329621

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