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7.5 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 7.5 · T2 T1 11.8795 dimensionless · rho2 rho1 5.5102 dimensionless · p2 p1 65.4583 dimensionless · M2 0.394907 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 7.5
M2 (dimensionless): 0.394907
T2 T1 (dimensionless): 11.879475
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.011329
P2 P1 (dimensionless): 65.458333
RHO2 RHO1 (dimensionless): 5.510204

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