Experiment on aerodynamic characteristics of a novel micro tilt ducted fan aircraft with wings

被引：0
|
作者：
Cai, Hong-Ming [1 ]
Ang, Hai-Song [1 ]
Zhang, Hua-Liang [1 ]
Duan, Wen-Bo [1 ]
机构：
[1] College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
来源：
Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica | 2012年 / 30卷 / 06期
关键词：
Aerodynamics; -; Fans;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Wind tunnel experiment is employed to study the aerodynamic characteristics of a novel micro tilt ducted fan MAV. Full-scale model is adopted in the wind tunnel experiment. The experiment focus on three modes: no motor, single motor and dual motors, respectively. The influences of design parameters on aerodynamic forces and moments are measured to get some typical aerodynamic characteristics. The test results are useful for theoretical modeling.
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页码：777 / 781
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