Analysis of the aerodynamic configuration of an aircraft for the control of the linear infrastructure

Authors

  • Ivanov Kirill Vladimirovich Ufa University of Science and Technology
  • Dudin Vadim Andreevich Ufa University of Science and Technology
  • Senyushkin Nikolay Sergeevich Ufa University of Science and Technology

Keywords:

unmanned aerial vehicle, gas dynamic calculation, digital twin, airframe, aerodynamic quality, software package, Ansys

Abstract

The article describes the process of preparing and calculating a digital model of an unmanned aerial vehicle (UAV) for vertical takeoff and landing in the Ansys CFX software package. The calculation result for one of the flight modes is given. The calculation results were processed in all flight modes. The analysis of the obtained results was carried out.

Author Biographies

Ivanov Kirill Vladimirovich, Ufa University of Science and Technology

1st year Master’s student specializing in thermal engineering and thermal power engineering, Faculty of Aircraft Engines, Power Engineering and Transport

Dudin Vadim Andreevich, Ufa University of Science and Technology

4th year student specializing in the design of aircraft and rocket engines, Faculty of Aircraft Engines, Power Engineering and Transport

Senyushkin Nikolay Sergeevich, Ufa University of Science and Technology

Acting Head of the Department of Thermal Engineering and Thermal Power Engineering, Candidate of Technical Sciences, Associate Professor at the Department of Thermal Engineering and Thermal Power Engineering, Faculty of Aircraft Engines, Power Engineering and Transpo

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Published

2024-15-08

Issue

Vol. 28 No. 2(104) (2024)

Section

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