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3.3 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 3.3 · T2 T1 3.04919 dimensionless · rho2 rho1 4.11202 dimensionless · p2 p1 12.5383 dimensionless · M2 0.459586 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 3.3
M2 (dimensionless): 0.459586
T2 T1 (dimensionless): 3.049191
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.253276
P2 P1 (dimensionless): 12.538333
RHO2 RHO1 (dimensionless): 4.11202

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