Study on Flight Performance of Propeller-Driven UAV

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ID: 40388
2019
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Abstract
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.
Reference Key
liu2019studyinternational Use this key to autocite in the manuscript while using SciMatic Manuscript Manager or Thesis Manager
Authors Liu, Rui-lin;Zhang, Zhong-jie;Jiao, Yu-fei;Yang, Chun-hao;Zhang, Wen-jian;
Journal international journal of aerospace engineering
Year 2019
DOI
DOI not found
URL
http://dx.doi.org/10.1155/2019/6282451
Keywords Keywords not found

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