Study of characteristics of vortex tube

Authors

  • Viktor Ivanovich Kuznetsov Omsk State Technical University, Omsk, Russia
  • Vladimir Vyacheslavovich Makarov Omsk State Technical University, Omsk, Russia
  • Aleksandr Sergeyevich Gritsay Omsk State Technical University, Omsk, Russia

DOI:

https://doi.org/10.25206/2588-0373-2022-6-2-85-89

Keywords:

thermogasodynamic characteristics, viscosity, tangential stresses, temperature efficiency

Abstract

Based on the previously compiled physical and mathematical model of the vortex tube workflow, the calculation
of the thermogasodynamic characteristics of the vortex tube with known geometric dimensions and their comparison
with experimental data was carried out. The calculations take into account the exchange of work and heat between
the axial and peripheral gas layers. The exchange of work is carried out due to the transfer of kinematic energy from
the axis to the periphery by viscosity forces when tangential stresses occur. The difference of thermodynamic
temperatures when heat is supplied from the periphery to the axis is taken into account. These phenomena reduce
the cooling effect of the flow coming out of the diaphragm.

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Author Biographies

Viktor Ivanovich Kuznetsov, Omsk State Technical University, Omsk, Russia

Doctor of Technical Sciences, Professor of Aviation and Rocketry Department, Omsk State Technical University (OmSTU), Omsk.

Vladimir Vyacheslavovich Makarov, Omsk State Technical University, Omsk, Russia

Candidate of Technical Sciences, Associate Professor of Aviation and Rocketry Department, OmSTU, Omsk.

Aleksandr Sergeyevich Gritsay, Omsk State Technical University, Omsk, Russia

Candidate of Technical Sciences, Associate Professor, Head of Computer Science and Computer Technology Department, OmSTU, Omsk.

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Abstract views: 17

Published

2022-06-21

How to Cite

Kuznetsov В. И., Makarov В. В., & Gritsay А. С. (2022). Study of characteristics of vortex tube. Omsk Scientific Bulletin. Series «Aviation-Rocket and Power Engineering», 6(2), 85–89. https://doi.org/10.25206/2588-0373-2022-6-2-85-89

Issue

Section

Aviation and rocket-space engineering

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