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Development of Unmanned Cargo VTOL Aircraft

  • Silesian University of Technology

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Citation (Scopus)

Abstract

The aim of the paper is to present a design cycle regarding to the construction of an unmanned cargo aircraft with own weight up to 25 kg, operating range of up to 100 km and AGL operating ceiling of up to 1 km. The task of the project team was to plan the design cycle, perform analytical calculations and CFD simulations, and finally to build an unmanned aircraft capable of lifting cargo. At the same time, a number of assumptions and technical regulations regarding constructions had to be met, which are specified in legal regulations regarding the given class of unmanned aerial vehicles. In order to achieve optimal UAV aerodynamic properties, including maximization of the payload while minimizing the own weight, aerodynamic calculations and CFD simulations were performed.

Original languageEnglish
Title of host publicationModelling in Engineering 2020
Subtitle of host publicationApplied Mechanics -
EditorsArkadiusz Mężyk, Sławomir Kciuk, Roman Szewczyk, Sławomir Duda
PublisherSpringer Science and Business Media Deutschland GmbH
Pages31-42
Number of pages12
ISBN (Print)9783030684549
DOIs
Publication statusPublished - 2021
Event59th Symposium on Engineering Modelling in Mechanics, 2020 - Gliwice, Poland
Duration: 22 Feb 202026 Feb 2020

Publication series

NameAdvances in Intelligent Systems and Computing
Volume1336
ISSN (Print)2194-5357
ISSN (Electronic)2194-5365

Conference

Conference59th Symposium on Engineering Modelling in Mechanics, 2020
Country/TerritoryPoland
CityGliwice
Period22/02/2026/02/20

Keywords

  • CFD
  • UAV
  • VTOL

ASJC Scopus subject areas

  • Control and Systems Engineering
  • General Computer Science

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