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5.5 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 5.5 · T2 T1 6.8218 dimensionless · rho2 rho1 5.14894 dimensionless · p2 p1 35.125 dimensionless · M2 0.408974 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 5.5
M2 (dimensionless): 0.408974
T2 T1 (dimensionless): 6.821798
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.042361
P2 P1 (dimensionless): 35.125
RHO2 RHO1 (dimensionless): 5.148936

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