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2.75 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 2.75 · T2 T1 2.39656 dimensionless · rho2 rho1 3.61194 dimensionless · p2 p1 8.65625 dimensionless · M2 0.49181 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 2.75
M2 (dimensionless): 0.49181
T2 T1 (dimensionless): 2.396565
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.406226
P2 P1 (dimensionless): 8.65625
RHO2 RHO1 (dimensionless): 3.61194

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