Using Wing Tip Devices to Improve Performance of Saucer-Shaped Aircraft-Reference-Cited by-同舟云学术

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Using Wing Tip Devices to Improve Performance of Saucer-Shaped Aircraft

Published:2006-11 Issue:4 Volume:19 Page:309-314
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

YU Jun-li,WANG Lin-lin,GAO Ge

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference4 articles.

1. Joel M G, Matthew T K. Development of the Black Widow micro air vehicle[R]. AIAA-2001–0127, 2001.

2. Data optimization and wind tunnel test of UAV winglets[J];Wu;Flight Dynamics,2004

3. Experimental research of the configuration of wing-tip drag reducing for light aircraft[J];Deng;Acta Aeronoutica et Astronautica Sinica,1994

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Parametric Study of Fluid Injection Winglet on Aerodynamic Performance of the Wing;Journal of Fluid Flow, Heat and Mass Transfer;2022

2. Optimization and analysis of winglet configuration for solar aircraft;Chinese Journal of Aeronautics;2020-12

3. Disturbance and Uncertainty Suppression Control for a Saucer-Shaped Unmanned Aerial Vehicle Based on Extended State Observer;Applied Sciences;2020-07-16

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