Email this article A Technique for Shortening Landing Run Distance of an Aircraft by Symmetrical Deflection of Split Elevator and Rudder
- Authors: Bazuhair M.A.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 61, No 2 (2018)
- Pages: 187-193
- Section: 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
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Abstract
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.
About the authors
M. A. Bazuhair
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: mohammed-ba@yandex.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
