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
Views 2044 Downloads 95
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
Follow on us
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.
Winglets, Structure, Flight Controls, Balancing, Design
To cite this article
Developing of Balancing Tools for Flight Controls, Automation, Control and Intelligent Systems.
Vol. 5, No. 6,
2017, pp. 92-95.
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.
Falcao, L.: Gomes, A. and Suleman, A. “Multidisciplinary design optimisation of a morphing wingtip.” In: 2nd International Conference on Engineering Optimization, Lisbon, Portugal, 6–9 September, 2010.
Hoerner, S. “The Aerodynamic Shape of the Wing Tips.” Dayton, OH: Air Materiel Command, Wright-Patterson Air Force Base, 1952.
Bower R.: “Opportunities for Aerodynamic-Drag Reduction. NASA SP-372. In: NASA/University conference on astronautics, University of Kansas, Lawrence, Kansas, October 23th, 1974, pp. 323–352.
Flechner, S., Jacobs, P., and Whithcomb, R. A. “High Subsonic Speed Wind-Tunnel Investigation of Winglets on a Representative Second-Generation Jet Transport Wing (NASA TN D-8264).” Washington, DC: NASA, 1976.
Whithcomb, R.: “A Design Approach and Selected Windtunnel Results at High Subsonic Speeds for Wing-Tip Mounted Winglets.” National Aeronautics and Space Administration Technical Note. NASA TN D-8260, 1976.
Williams, A. L.: “A New and Less Complex Alternative to the Handley Page Slat.” Technical Paper, Northrop Corp, 1985.