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...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Panayotov, Hristian, Penchev, Stanimir, Kolibarov, Dancho
Format: Tagungsbericht
Sprache:eng
Schlagworte:
Aerodynamic characteristics
Aerodynamics
Aircraft
Aircraft performance
Canard configurations
Mathematical models
Numerical methods
Rapid prototyping
Three dimensional printing
Unmanned aerial vehicles
Unmanned aircraft
Wind tunnels
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung: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.
ISSN:2261-236X
2274-7214
2261-236X
DOI:10.1051/matecconf/201713301002