Study on Flight Performance of Propeller-Driven UAV
Joint Authors
Liu, Rui-lin
Zhang, Zhong-jie
Jiao, Yu-fei
Yang, Chun-hao
Zhang, Wen-jian
Source
International Journal of Aerospace Engineering
Issue
Vol. 2019, Issue 2019 (31 Dec. 2019), pp.1-11, 11 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2019-04-21
Country of Publication
Egypt
No. of Pages
11
Abstract EN
The engine performance test at altitudes of 0-7000 m was carried out on the high-performance test bench of the Unmanned Aerial Vehicle (UAV) piston engine.
The flight performance of UAV was studied, including propeller thrust characteristics, maneuverability, flight envelope, and cruise performance.
The results showed that with the increase in altitudes, the UAV climb rate gradually decreased; the maximum climb rate decreased from 2.5 m/s at 2000 m to 0.5 m/s at 7000 m.
The maximum flight altitude is 7000 m, and the flight speed range is about 47 m/s-52 m/s at the altitude of 7000 m.
Maximum navigation range and endurance of UAV decrease by 5.8% and 8%, respectively, with each increment of 1000 m in altitudes.
American Psychological Association (APA)
Liu, Rui-lin& Zhang, Zhong-jie& Jiao, Yu-fei& Yang, Chun-hao& Zhang, Wen-jian. 2019. Study on Flight Performance of Propeller-Driven UAV. International Journal of Aerospace Engineering،Vol. 2019, no. 2019, pp.1-11.
https://search.emarefa.net/detail/BIM-1156778
Modern Language Association (MLA)
Liu, Rui-lin…[et al.]. Study on Flight Performance of Propeller-Driven UAV. International Journal of Aerospace Engineering No. 2019 (2019), pp.1-11.
https://search.emarefa.net/detail/BIM-1156778
American Medical Association (AMA)
Liu, Rui-lin& Zhang, Zhong-jie& Jiao, Yu-fei& Yang, Chun-hao& Zhang, Wen-jian. Study on Flight Performance of Propeller-Driven UAV. International Journal of Aerospace Engineering. 2019. Vol. 2019, no. 2019, pp.1-11.
https://search.emarefa.net/detail/BIM-1156778
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1156778
