The heating and cooling in a vortex tube is attributed to conversion o
f kinetic energy into heat and to the reverse process. A two-component
model yields the upper limit for the temperature increase on the hot
side: (T(h) - T0)/T0 less-than-or-equal-to X(gamma - 1)/gamma, and a l
ower limit for the temperature reduction on the cold side: T(c) greate
r-than-or-equal-to T0(1 - X)(gamma-1)/gamma, where gamma = 1.4 for air
, and X = (p0 - p(c))/p0 is the normalized pressure drop between the i
nlet (p0) and the cold exhaust port (p(c)). Extensive experimental dat
a for a vortex tube of 18 mm inner diameter with working fluid air all
fall between these limits. The model predicts that the inlet velocity
reaches the speed of sound for X = 0.7. No values X > 0.7 could be ob
tained in these experiments, indicating that the flow always remain su
bsonic.