Experimental study of canard UAV aerodynamics

Experimental study of canard UAV aerodynamics

The present paper presents the aerodynamic characteristics of a canard fixed-wing unmanned aircraft TERES-02. A wind tunnel experiment is conducted using a specially designed model of the aircraft. The model is produced through the methods of rapid prototyping using a FDM 3D printer. Aerodynamic cor...

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Bibliographic Details
Main Authors: Panayotov Hristian, Penchev Stanimir, Kolibarov Dancho
Format: Article
Language:English
Published: EDP Sciences 2017-01-01
Series:MATEC Web of Conferences
Online Access:https://doi.org/10.1051/matecconf/201713301002
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spelling doaj-1bbca9f139b04110aecb970659d84a552021-02-02T01:04:15ZengEDP SciencesMATEC Web of Conferences2261-236X2017-01-011330100210.1051/matecconf/201713301002matecconf_bultrans2017_01002Experimental study of canard UAV aerodynamicsPanayotov HristianPenchev StanimirKolibarov DanchoThe present paper presents the aerodynamic characteristics of a canard fixed-wing unmanned aircraft TERES-02. A wind tunnel experiment is conducted using a specially designed model of the aircraft. The model is produced through the methods of rapid prototyping using a FDM 3D printer. Aerodynamic corrections are made and thorough analysis and discussion of the results is carried out. The obtained results can be used to determine the accuracy of numerical methods for analysis of aircraft performance.https://doi.org/10.1051/matecconf/201713301002
collection DOAJ
language English
format Article
sources DOAJ
author Panayotov Hristian
Penchev Stanimir
Kolibarov Dancho
spellingShingle Panayotov Hristian
Penchev Stanimir
Kolibarov Dancho
Experimental study of canard UAV aerodynamics
MATEC Web of Conferences
author_facet Panayotov Hristian
Penchev Stanimir
Kolibarov Dancho
author_sort Panayotov Hristian
title Experimental study of canard UAV aerodynamics
title_short Experimental study of canard UAV aerodynamics
title_full Experimental study of canard UAV aerodynamics
title_fullStr Experimental study of canard UAV aerodynamics
title_full_unstemmed Experimental study of canard UAV aerodynamics
title_sort experimental study of canard uav aerodynamics
publisher EDP Sciences
series MATEC Web of Conferences
issn 2261-236X
publishDate 2017-01-01
description The present paper presents the aerodynamic characteristics of a canard fixed-wing unmanned aircraft TERES-02. A wind tunnel experiment is conducted using a specially designed model of the aircraft. The model is produced through the methods of rapid prototyping using a FDM 3D printer. Aerodynamic corrections are made and thorough analysis and discussion of the results is carried out. The obtained results can be used to determine the accuracy of numerical methods for analysis of aircraft performance.
url https://doi.org/10.1051/matecconf/201713301002
work_keys_str_mv AT panayotovhristian experimentalstudyofcanarduavaerodynamics
AT penchevstanimir experimentalstudyofcanarduavaerodynamics
AT kolibarovdancho experimentalstudyofcanarduavaerodynamics
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