| Autors: Panayotov, H. P., Penchev, S. I., Kolibarov, D. S. Title: Experimental study of canard UAV aerodynamics Keywords: aerodynamic experiment, wind tunnel, coefficients of lift, d 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. References Issue
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Цитирания (Citation/s):
1. [HTML] Low Observable Uncrewed Aerial Vehicle Wind Tunnel Model Design, Manufacturing, and Aerodynamic Characterization H Aleisa, K Kontis, M Nikbay - Aerospace, 2024 - mdpi.com - 2024 - в издания, индексирани в Scopus и/или Web of Science
2. Подходы к проектированию и практика применения беспилотных воздушных судов самолётного типа СВ Скоробогатов, ДА Бутуров - Crede Experto: транспорт …, 2023 - cyberleninka.ru - 2023 - от чужди автори в чужди издания, неиндексирани в Scopus или Web of Science
3. Experimental study of static characteristics of a helicopter rotor in ground effect G Georgiev, F Panayotov, V Serbezov… - AIP Conference …, 2024 - pubs.aip.org - 2024 - в издания, индексирани в Scopus и/или Web of Science
4. [PDF] Pavan N, UG Student, Department of Mechanical Engineering, REVA University, Bangalore 560064, India Prabhanjan Kamte, UG Student, Department of … BP Madhu, R Girish - journal-dogorangsang.in - 2022 - от чужди автори в чужди издания, неиндексирани в Scopus или Web of Science
Вид: публикация в международен форум, публикация в реферирано издание, индексирана в Scopus
