The heating and cooling in a vortex tube is attributed to conversion of 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 -To)/T 0 or=T 0 (1-X) ( gamma -1 / gamma ), where gamma =1.4 for air, and X=(p 0 -p c )/p 0 is the normalized pressure drop between the inlet (p 0 ) and the cold exhaust port (Pc) Extensive experimental data 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 obtained in these experiments, indicating that the flow always remain subsonic.
No takes yet. Share an insight, caveat, or question.
Ahlborn et al. (1994) studied this question.
Synapse has enriched 5 related papers. Consider them for comparative context: