Experimental Studies of X-47B-type Unmanned Aerial Vehicle in TsAGI T-102 Wind Tunnel to Assess Effectiveness of Aerodynamic Controls in Longitudinal Channel
- 作者: Krivoshchapov A.1
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隶属关系:
- Zhukovsky Central Aerohydrodynamics Institute (TsAGI)
- 期: 卷 62, 编号 2 (2019)
- 页面: 342-347
- 栏目: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230993
- DOI: https://doi.org/10.3103/S1068799819020247
- ID: 230993
如何引用文章
详细
The results are given on the experimental studies of integral aerodynamic characteristics of X-47B-type “flying wing” unmanned aerial vehicle model. The dependence of the lift coefficient on the angle of attack for different trimmings and static margin is evaluated. It is shown that rational combination of aerodynamic surface deflections allows increasing sufficiently the trimmed lift coefficient values for take-off and landing flight regimes.
作者简介
A. Krivoshchapov
Zhukovsky Central Aerohydrodynamics Institute (TsAGI)
编辑信件的主要联系方式.
Email: alex5000.89@mail.ru
俄罗斯联邦, ul. Zhukovskogo 1, Zhukovsky, 140181