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2.9 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 2.9 · T2 T1 2.56321 dimensionless · rho2 rho1 3.76286 dimensionless · p2 p1 9.645 dimensionless · M2 0.48138 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 2.9
M2 (dimensionless): 0.48138
T2 T1 (dimensionless): 2.563207
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.357733
P2 P1 (dimensionless): 9.645
RHO2 RHO1 (dimensionless): 3.762864

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