Developing of Balancing Tools for Flight Controls

Anas Tharakath; Konstantin Nechval

doi:doi:10.11648/j.acis.20170506.12

| Peer-Reviewed

Developing of Balancing Tools for Flight Controls

Anas Tharakath, Konstantin Nechval

Published in Automation, Control and Intelligent Systems (Volume 5, Issue 6)

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

Views: Downloads:

Download PDF

Share This Article

Twitter
Linked In
Facebook

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

Plain Text BibTeX RIS

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

Copy | Download

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

Copy | Download

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

Copy | Download

@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}
}

Copy | Download

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  -

Copy | Download

Author Information

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

Download PDF

Sections

Plain Text BibTeX RIS

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

Copy | Download

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

Copy | Download

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

Copy | Download

@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}
}

Copy | Download

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  -

Copy | Download