A Technique for Shortening Landing Run Distance of an Aircraft by Symmetrical Deflection of Split Elevator and Rudder
- 作者: Bazuhair M.1
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隶属关系:
- Tupolev Kazan National Research Technical University
- 期: 卷 61, 编号 2 (2018)
- 页面: 187-193
- 栏目: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230480
- DOI: https://doi.org/10.3103/S106879981802006X
- ID: 230480
如何引用文章
详细
In this work, we investigate an application of symmetrical deflection of the split elevators and rudder up to 45 degrees to function as air-brakes during landing run for shortening its distance. A computational analysis for the landing run under standard atmospheric conditions is conducted. The effect of the proposed solution on the aircraft structure and performance was studied.
作者简介
M. Bazuhair
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: mohammed-ba@yandex.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111