Abstract
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.
Cite
CITATION STYLE
Panayotov, H., Penchev, S., & Kolibarov, D. (2017). Experimental study of canard UAV aerodynamics. In MATEC Web of Conferences (Vol. 133). EDP Sciences. https://doi.org/10.1051/matecconf/201713301002
Register to see more suggestions
Mendeley helps you to discover research relevant for your work.
