Numerical Investigation and Aerodynamic Configuration Optimisation of a VTOL Flying Wing UAV
By: V. Gopejenko, N. Sidenko and R. I. Mukhamediev
Authors
V. Gopejenko
Ventspils University of Applied Sciences, International Radio Astronomy Centre, Ventspils, Latvia
Riga Nordic University, Department of Natural Science and Computer Technologies, Riga, Latvia
N. Sidenko
Riga Technical University, Faculty of Civil and Mechanical Engineering, Institute of Sustainable Building Materials and Engineering Systems, Riga, Latvia
R. I. Mukhamediev
Institute of Automation and Information Technologies, Department of Software Engineering, Satbayev University (Kazakh National Research Technical University named after K.I. Satpayev), Almaty, Kazakhstan
DOI: https://doi.org/10.2478/lpts-2026-0027 | Journal eISSN: 2255-8896 (formerly 0868-8257) | Journal ISSN: 0868-8257
Language: English
Page range: 26 - 47
Published on: Aug 6, 2026
Published by: Institute of Physical Energetics
In partnership with: Paradigm Publishing Services
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© 2026 V. Gopejenko, N. Sidenko, R. I. Mukhamediev, published by Institute of Physical Energetics
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.