Andriy Avramenko

Institute of Engineering Thermophysics of NAS of Ukraine, Ukraine
Doctor of Technical Sciences, Professor
Department heat and mass transfer and hydrodynamics in heat power equipment

Scopus profile: link
Researcher ID: J-2915-2014
Google Scholar profile: link
ID ORCID: https://orcid.org/0000-0002-2416-3512

Selected Publications:

  1. Avramenko, A. A., Shevchuk, I. V., Kovetskaya, M. M., Kovetska, Y. Y., Anastasiev, D. V. (2025). Analysis of the Limiting Values of Thermodynamic Parameters for Jouguet Detonation. Mathematics, 13 (15), 2419. https://doi.org/10.3390/math13152419 
  2. Avramenko, A. A., Shevchuk, I. V., Tyrinov, A. I., Dzevulska, I. V. (2025). Numerical Simulation of Cytokinesis Hydrodynamics. Computation, 13 (7), 163. https://doi.org/10.3390/computation13070163 
  3. Avramenko, A. A., Shevchuk, I. V., Kobzar, A. S. (2025). Discrete Symmetry Analysis of Free Convection in a Cylindrical Porous Annular Microchannel at Low-Pressure Level. ASME Journal of Heat and Mass Transfer, 147 (6). https://doi.org/10.1115/1.4067609 
  4. Avramenko, A. A., Tyrinov, A. I., Kovetska, Y. Y., Kobzar, A. S. (2025). Investigation of heat generation and flow of viscous electron fluid in rectangular conductors. International Communications in Heat and Mass Transfer, 165, 108988. https://doi.org/10.1016/j.icheatmasstransfer.2025.108988 
  5. Avramenko, A. A., Shevchuk, I. V., Dmitrenko, N. P., Konyk, A. V. (2025). Renormalization Group Approach as a Symmetry Transformation for an Analysis of Non-Newtonian Elastic Turbulence. Fluids, 10 (4), 79. https://doi.org/10.3390/fluids10040079 
  6. Avramenko, A. A., Shevchuk, I. V., Dmitrenko, N. P., Tyrinov, A. I., Kovetska, Y. Y., Kobzar, A. S. (2025). Oscillation Flow of Viscous Electron Fluids in Conductors of Rectangular Cross-Section. Computation, 13 (4), 90. https://doi.org/10.3390/computation13040090 
  7. Avramenko, A. A., Shevchuk, I. V., Kovetskaya, M. M., Kovetska, Y. Y., Tyrinov, A. I., Anastasiev, D. V. (2025). Transformation of Perturbations in Supersonic Gas Flow Subject to Oblique Shock Wave. Aerospace, 12 (4), 323. https://doi.org/10.3390/aerospace12040323