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6.5 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 6.5 · T2 T1 9.15644 dimensionless · rho2 rho1 5.36508 dimensionless · p2 p1 49.125 dimensionless · M2 0.400381 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 6.5
M2 (dimensionless): 0.400381
T2 T1 (dimensionless): 9.156435
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.021148
P2 P1 (dimensionless): 49.125
RHO2 RHO1 (dimensionless): 5.365079

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