Developing of Balancing Tools for Flight Controls
Automation, Control and Intelligent Systems
Volume 5, Issue 6, December 2017, Pages: 92-95
Received: Sep. 20, 2017; Accepted: Oct. 13, 2017; Published: Nov. 29, 2017
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Authors
Anas Tharakath, Transport and Telecommunication Institute, Transport and Logistic Faculty, Department of Aviation Transport, Riga, Latvia
Konstantin Nechval, Transport and Telecommunication Institute, Transport and Logistic Faculty, Department of Aviation Transport, Riga, Latvia
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Abstract
Wingtip devices may be fitted for various reasons, they often combine more than one function and usually occupy a substantial part of the stabilizer, just belong the aileron spar. Winglets allow decreasing fuel consumption of over 10%. But with the development of new generations of aircraft, it is not always appropriate to take into account the stability and controllability of the flight. Because there is a need to improve the existing designs in the paper proposed new concept of winglets.
Keywords
Winglets, Structure, Flight Controls, Balancing, Design
To cite this article
Anas Tharakath, Konstantin Nechval, Developing of Balancing Tools for Flight Controls, Automation, Control and Intelligent Systems. Vol. 5, No. 6, 2017, pp. 92-95. doi: 10.11648/j.acis.20170506.12
Copyright
Copyright © 2017 Authors retain the copyright of this article.
This article is an open access article distributed under the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0/) which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
References
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