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Developing of Balancing Tools for Flight Controls

Received: 20 September 2017     Accepted: 13 October 2017     Published: 29 November 2017
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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.

Published in Automation, Control and Intelligent Systems (Volume 5, Issue 6)
DOI 10.11648/j.acis.20170506.12
Page(s) 92-95
Creative Commons

This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.

Copyright

Copyright © The Author(s), 2017. Published by Science Publishing Group

Keywords

Winglets, Structure, Flight Controls, Balancing, Design

References
[1] 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.
[2] Hoerner, S. “The Aerodynamic Shape of the Wing Tips.” Dayton, OH: Air Materiel Command, Wright-Patterson Air Force Base, 1952.
[3] 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.
[4] 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.
[5] 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.
[6] Williams, A. L.: “A New and Less Complex Alternative to the Handley Page Slat.” Technical Paper, Northrop Corp, 1985.
Cite This Article
  • APA Style

    Anas Tharakath, Konstantin Nechval. (2017). Developing of Balancing Tools for Flight Controls. Automation, Control and Intelligent Systems, 5(6), 92-95. https://doi.org/10.11648/j.acis.20170506.12

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    ACS Style

    Anas Tharakath; Konstantin Nechval. Developing of Balancing Tools for Flight Controls. Autom. Control Intell. Syst. 2017, 5(6), 92-95. doi: 10.11648/j.acis.20170506.12

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    AMA Style

    Anas Tharakath, Konstantin Nechval. Developing of Balancing Tools for Flight Controls. Autom Control Intell Syst. 2017;5(6):92-95. doi: 10.11648/j.acis.20170506.12

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  • @article{10.11648/j.acis.20170506.12,
      author = {Anas Tharakath and Konstantin Nechval},
      title = {Developing of Balancing Tools for Flight Controls},
      journal = {Automation, Control and Intelligent Systems},
      volume = {5},
      number = {6},
      pages = {92-95},
      doi = {10.11648/j.acis.20170506.12},
      url = {https://doi.org/10.11648/j.acis.20170506.12},
      eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.acis.20170506.12},
      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.},
     year = {2017}
    }
    

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  • TY  - JOUR
    T1  - Developing of Balancing Tools for Flight Controls
    AU  - Anas Tharakath
    AU  - Konstantin Nechval
    Y1  - 2017/11/29
    PY  - 2017
    N1  - https://doi.org/10.11648/j.acis.20170506.12
    DO  - 10.11648/j.acis.20170506.12
    T2  - Automation, Control and Intelligent Systems
    JF  - Automation, Control and Intelligent Systems
    JO  - Automation, Control and Intelligent Systems
    SP  - 92
    EP  - 95
    PB  - Science Publishing Group
    SN  - 2328-5591
    UR  - https://doi.org/10.11648/j.acis.20170506.12
    AB  - 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.
    VL  - 5
    IS  - 6
    ER  - 

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Author Information
  • Transport and Telecommunication Institute, Transport and Logistic Faculty, Department of Aviation Transport, Riga, Latvia

  • Transport and Telecommunication Institute, Transport and Logistic Faculty, Department of Aviation Transport, Riga, Latvia

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