Physics and mathematics model of vortex tube working process

Authors

  • Viktor Ivanovich Kuznetsov Omsk State Technical University, Omsk, Russia
  • Vladimir Vyacheslavovich Makarov Omsk State Technical University, Omsk, Russia
  • Aleksandra Yuriyevna Shander Omsk State Technical University, Omsk, Russia

DOI:

https://doi.org/10.25206/2588-0373-2021-5-2-78-87

Keywords:

vortex tube, compression energy, expansion energy, work exchange, heat exchange

Abstract

Based on the physical model of the Ranque effect, proposed earlier, a simplified mathematical model of the working process
of a vortex tube is compiled taking into account the exchange of work and heat during the interaction of peripheral and axial gas flows. The effect of viscosity and angular velocity gradient on the transfer of kinetic energy from the axis to the periphery is shown. The difference in thermodynamic temperatures when heat is supplied from the periphery to the axis is taken into account, which leads to a decrease in the cooling efficiency of the axial gas flow. Energy exchange is based on the assumption that the peripheral gas layers are compressed by the axial flow. The axial flow work is determined by the pressure difference between the valve and the outlet of the diaphragm.

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Author Biographies

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

Doctor of Technical Sciences, Professor of Aircraft and Rocket Building Department.

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

Candidate of Technical Sciences, Associate Professor of Aircraft and Rocket Building Department.

Aleksandra Yuriyevna Shander, Omsk State Technical University, Omsk, Russia

Assistant of Aircraft and Rocket Building Department.

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Abstract views: 7

Published

2021-06-30

How to Cite

Kuznetsov В. И., Makarov В. В., & Shander А. Ю. (2021). Physics and mathematics model of vortex tube working process. Omsk Scientific Bulletin. Series «Aviation-Rocket and Power Engineering», 5(2), 78–87. https://doi.org/10.25206/2588-0373-2021-5-2-78-87

Issue

Section

Aviation and rocket-space engineering