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1.75 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 1.75 · T2 T1 1.49458 dimensionless · rho2 rho1 2.27907 dimensionless · p2 p1 3.40625 dimensionless · M2 0.628089 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 1.75
M2 (dimensionless): 0.628089
T2 T1 (dimensionless): 1.494579
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.834565
P2 P1 (dimensionless): 3.40625
RHO2 RHO1 (dimensionless): 2.27907

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