Mathematical analysis of propeller flight simulation

DOI

10.2991/978-94-6463-423-5_14How to use a DOI?

Keywords

drone; propeller; mathematical analysis; aerodynamic lift force

Abstract

The thesis focuses on the analysis and calculation of the aerodynamic lift force of the propeller that is applied to the drone. The unmanned aerial vehicle, a drone, can be remotely controlled or capable of autonomous flight using pre-programmed flight plans or more complex dynamic autonomous systems. The main input is a model of the propeller, in this particular case a model of the three-bladed propeller that is used on the drone. The thesis summarizes the theoretical knowledge of the physics of flight. Subsequent analysis and mathematical calculation establishes the dependence of the lift force on the rotation of the propeller, which is shown in the table. The result of the work is the maximum load that the propeller can sustain in the process of flight due to the aerodynamic lift force.

Copyright

© 2024 The Author(s)

Open Access

Open Access This chapter is licensed under the terms of the Creative Commons Attribution-NonCommercial 4.0 International License (http://creativecommons.org/licenses/by-nc/4.0/), which permits any noncommercial use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license and indicate if changes were made.

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TY  - CONF
AU  - Jakub Fiačan
AU  - Slavomír Hrček
AU  - František Brumerčík
AU  - Jozef Ondriga
AU  - Ján Steininger
AU  - Pavol Michal
AU  - Zdenko Šavrnoch
PY  - 2024
DA  - 2024/05/22
TI  - Mathematical analysis of propeller flight simulation
BT  - Proceedings of the 62nd International Conference of Machine Design Departments (ICMD 2022)
PB  - Atlantis Press
SP  - 123
EP  - 131
SN  - 2589-4943
UR  - https://doi.org/10.2991/978-94-6463-423-5_14
DO  - 10.2991/978-94-6463-423-5_14
ID  - Fiačan2024
ER  -