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3.9 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 3.9 · T2 T1 3.89281 dimensionless · rho2 rho1 4.51559 dimensionless · p2 p1 17.5783 dimensionless · M2 0.437742 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 3.9
M2 (dimensionless): 0.437742
T2 T1 (dimensionless): 3.892813
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.151027
P2 P1 (dimensionless): 17.578333
RHO2 RHO1 (dimensionless): 4.515586

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