Study on design of low Reynolds number reflexed airfoil for solar-powered UAV in flying wing configuration
Based on the application requirements of a small hand-launched solar-powered unmanned aerial vehicle (UAV) in flying wing configuration, the optimization design of the low Reynolds number (LRN) reflexed airfoil is carried out in this study to meet several requirements such as high lift, mild stall,...
Main Authors: | WANG Kelei, ZHOU Zhou, GUO Jiahao, XU De |
---|---|
Format: | Article |
Language: | zho |
Published: |
EDP Sciences
2022-06-01
|
Series: | Xibei Gongye Daxue Xuebao |
Subjects: | |
Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2022/03/jnwpu2022403p512/jnwpu2022403p512.html |
Similar Items
-
Study on design characteristics of airfoil pressure distribution for low Mach number general aircraft
by: ZHANG Yu, et al.
Published: (2023-02-01) -
Lateral attitude control of solar-powered UAV with high aspect ratio
by: WANG Bo, et al.
Published: (2022-12-01) -
Influence of geometric parameters of leading edge horn-ice on stall characteristics of airfoil
by: ZHAO Binbin, et al.
Published: (2023-02-01) -
A wall-modelled large eddy simulation approach based on large scale parallel computing for post stall flow over an iced airfoil
by: LI Li, et al.
Published: (2023-10-01) -
Study on circulation control of flying wing based on Coanda effect
by: LIU Xiaodong, et al.
Published: (2022-08-01)