Normal Flow Relations

The calculator computes ratios to free stream values across a normal shock wave and compares pressure and temperature variations across a normal shock wave between given state 1 and state 2.

Select an input variable by using the choice button and then type in the value of the selected variable.

In region “2” the fluid element at rest have total pressure and total temperature p0,2 and T2 respectively.

For perfect gas, γ =
angles in degrees

M1 =

p2/p1 =

M2 =

ρ21 =

p02/p01 =

T2/T1 =

p1/p02 =