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2.1 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 2.1 · T2 T1 1.77045 dimensionless · rho2 rho1 2.8119 dimensionless · p2 p1 4.97833 dimensionless · M2 0.561277 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 2.1
M2 (dimensionless): 0.561277
T2 T1 (dimensionless): 1.77045
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.674203
P2 P1 (dimensionless): 4.978333
RHO2 RHO1 (dimensionless): 2.811902

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