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2.2 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 2.2 · T2 T1 1.85686 dimensionless · rho2 rho1 2.95122 dimensionless · p2 p1 5.48 dimensionless · M2 0.547056 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 2.2
M2 (dimensionless): 0.547056
T2 T1 (dimensionless): 1.85686
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.628136
P2 P1 (dimensionless): 5.48
RHO2 RHO1 (dimensionless): 2.95122

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