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4.1 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 4.1 · T2 T1 4.20479 dimensionless · rho2 rho1 4.62448 dimensionless · p2 p1 19.445 dimensionless · M2 0.432363 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 4.1
M2 (dimensionless): 0.432363
T2 T1 (dimensionless): 4.204793
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.127556
P2 P1 (dimensionless): 19.445
RHO2 RHO1 (dimensionless): 4.624484

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