Explore the Engineering Database more efficiently by signing up for free. Sign up free

3.1 — Normal Shock

Name: Compressible Flow — NORMAL_SHOCK: mach number 3.1 · T2 T1 2.7986 dimensionless · rho2 rho1 3.94661 dimensionless · p2 p1 11.045 dimensionless · M2 0.469534 dimensionless
Creator: Engineering Database

Flow Type: Normal Shock
Mach Number: 3.1
M2 (dimensionless): 0.469534
T2 T1 (dimensionless): 2.798603
Gamma (dimensionless): 1.4
P02 P01 (dimensionless): 0.301211
P2 P1 (dimensionless): 11.045
RHO2 RHO1 (dimensionless): 3.946612

Browse more mechanical engineering reference tables →