$ cd ..
Normal Shock
Compute M2, pressure ratios, and total-pressure loss from upstream Mach number.
visual calculatorCompressible Flow
Read the flow shape before trusting the number.
This page turns a CFD setup into regime, scale, and dominant-effect cues. Adjust the calculator below and compare the moving graphic with the computed result.
01
input scale
02
model
03
check
compressibleshocknormal shock
formula
KaTeX rendered
ASCII source
M2^2 = [1 + (gamma-1) M1^2 / 2] / [gamma M1^2 - (gamma-1) / 2]M12.000000
M20.577350
p2/p14.500000
ρ2/ρ12.666667
T2/T11.687500
p02/p010.720874
p1/p020.177291