Experimental investigation of lift for a wing-in-ground effect aircraft model
- 作者: Nazarov D.V.1, Frolov V.A.1, Shakhov V.G.1
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隶属关系:
- Samara University
- 期: 卷 59, 编号 2 (2016)
- 页面: 206-210
- 栏目: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/229661
- DOI: https://doi.org/10.3103/S1068799816020082
- ID: 229661
如何引用文章
详细
The aim of the investigation is to develop a technique of recalculating the lift as a function of the angle of attack at different reference points of the aircraft model height over the ground surface. A technique for evaluating the lift of the aircraft model close to the ground surface is proposed.
作者简介
D. Nazarov
Samara University
编辑信件的主要联系方式.
Email: dvn69@mail.ru
俄罗斯联邦, Moskovskoe shosse 34, Samara, 443086
V. Frolov
Samara University
Email: dvn69@mail.ru
俄罗斯联邦, Moskovskoe shosse 34, Samara, 443086
V. Shakhov
Samara University
Email: dvn69@mail.ru
俄罗斯联邦, Moskovskoe shosse 34, Samara, 443086
补充文件
