Detailed Information
Cited 0 time in 
Cited 0 time in 
Cited 0 time in
Metadata Downloads
DESIGN & FLIGHT TEST RESULT OF A SMALL SCALE HYBRID VTOL UAV소형 하이브리드 수직이착륙 무인기의 설계와 비행시험
- Other Titles
- 소형 하이브리드 수직이착륙 무인기의 설계와 비행시험
- Authors
- 김봉환; FOONG-YI CHIA; 민경무
- Issue Date
- Apr-2019
- Publisher
- TRANS STELLAR
- Citation
- International Journal of Mechanical and Production Engineering Research and Development , v.9, no.2, pp 203 - 210
- Pages
- 8
- Indexed
- SCOPUS
- Journal Title
- International Journal of Mechanical and Production Engineering Research and Development
- Volume
- 9
- Number
- 2
- Start Page
- 203
- End Page
- 210
- ISSN
- 2249-6890
2249-8001
- Abstract
- Installing a quadcopter in H-configuration onto the wings is one of the ways to introduce vertical flight to a fixed wing UAV. Forward flight is attained by tilting the motors to create forward thrust. This paper discusses the design considerations for the Hybrid VTOL UAV and presents the results from flight tests. The motors are electric and powered by Lithium-Polymer batteries. XFLR5 is used to calculate the aerodynamics variables of the design. Drag and flight endurance is calculated empirically and compared against the real values obtained from flight tests.
- Files in This Item
- There are no files associated with this item.
- Appears in
Collections - 융합기술공과대학 > Department of Automotive Engineering > Journal Articles
Items in ScholarWorks are protected by copyright, with all rights reserved, unless otherwise indicated.