Investigation on Aerodynamic Configuration of Monitoring Long Endurance UAV

Article Preview

Abstract:

In recent years, monitoring long endurance UAV is widely used in civil fields such as earthquake relief, it has certain particularities in comparison with conventional UAV; this paper studied and summarized its key technologies in aerodynamic configuration. The research of aerodynamic configuration is based on a general scheme, research indicates that: (1) monitoring long endurance UAV has the characteristics of low-Reynolds number, so laminar airfoil is needed to increase lift-drag ratio; induced drag can be reduced by optimizing wing twist angle; (2) subsection control surface and new design method on flight-quality would improve control reliability and flight quality, which are indispensable for the UAV to guarantee safety in bad weather condition; (3) take-off/landing/taxiing performance should be considered in order to improve the runway adaptability of the UAV.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

80-85

Citation:

Online since:

February 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Wang xin, Chen Wu. Discussion on prospects of low-altitude UAV remote sensing technology in the field of water conservancy. Zhejiang Hydrotechnics. 2010, No. 172.

Google Scholar

[2] Yan Ming, Su Xingyuan, et al. Prediction of transitional flows using an improved low-Reynolds-number turbulence model with transition sensitivity. Journal of Aerospace Power. 2009, Vol. 24 No. 12.

Google Scholar

[3] Bai Peng, Cui Erjie, et al. Numerical simulation of laminar separation bubble over 2D airfoil at low Reynolds number. ACTA AERODYNAMICA SINICA. 2006, Vol. 24 No. 4.

Google Scholar

[4] Weisheng Chen, Luis P. Bernal. Design and Performance of Low Reynolds Number Airfoils for Solar-Powered Flight AIAA-2008-316, (2008).

DOI: 10.2514/6.2008-316

Google Scholar

[5] Ma Tielin, Ma Dongli, et al. Aerodynamic characteristic analysis of high-aspect ratio elastic wing. Journal of Beijing University of Aeronautics and Astronautics. 2007, Vol. 33 No7.

Google Scholar

[6] Zhang Jianjun, Yang Shipu, et al. Study on aircraft lateral-directional character with different winglets. FLIGHT DYNAMICS. 2011, Vol. 29 No. 4.

Google Scholar

[7] Cui Yuwei, Zhang Weiguo. Research for multi-control-effector reconfigurable control based on linear programming. FLIGHT DYNAMICS. 2011, Vol. 29 No. 2.

Google Scholar