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Determination of Required Torque to Spin Aircraft Wheel at Approach Using ANSYS CFX

Received: 9 April 2016     Accepted: 20 April 2016     Published: 3 May 2016
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Abstract

Many patents have suggested that spinning the aircraft wheel before touchdown would lessen tyre wear as indicated by landing smoke and rubber deposites on the runway caused by skidding wheel at the point of impact. In this paper, the required torque to spin the aircraft wheel at approach speed has been calculated using ANSYS Workbench CFX, which is used to determine the wheel aerodynamic forces developed by simulation of fluid flows in a virtual environment. The wheel has been tested against different wind speeds, and the aerodynamic forces for the spinning wheel are presented, which include; translational and rotational drags, lift created by vortex, and shaft rolling resistance.

Published in American Journal of Aerospace Engineering (Volume 3, Issue 2)
DOI 10.11648/j.ajae.20160302.12
Page(s) 13-23
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), 2016. Published by Science Publishing Group

Keywords

Spinning Aircraft Wheel, Aerodynamic Force, Translational Drag, Rotational Drag, SST Turbulence RANS Model, ANSYS CFX

References
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Cite This Article
  • APA Style

    Abdurrhman A. Alroqi, Weiji Wang. (2016). Determination of Required Torque to Spin Aircraft Wheel at Approach Using ANSYS CFX. American Journal of Aerospace Engineering, 3(2), 13-23. https://doi.org/10.11648/j.ajae.20160302.12

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    ACS Style

    Abdurrhman A. Alroqi; Weiji Wang. Determination of Required Torque to Spin Aircraft Wheel at Approach Using ANSYS CFX. Am. J. Aerosp. Eng. 2016, 3(2), 13-23. doi: 10.11648/j.ajae.20160302.12

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    AMA Style

    Abdurrhman A. Alroqi, Weiji Wang. Determination of Required Torque to Spin Aircraft Wheel at Approach Using ANSYS CFX. Am J Aerosp Eng. 2016;3(2):13-23. doi: 10.11648/j.ajae.20160302.12

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  • @article{10.11648/j.ajae.20160302.12,
      author = {Abdurrhman A. Alroqi and Weiji Wang},
      title = {Determination of Required Torque to Spin Aircraft Wheel at Approach Using ANSYS CFX},
      journal = {American Journal of Aerospace Engineering},
      volume = {3},
      number = {2},
      pages = {13-23},
      doi = {10.11648/j.ajae.20160302.12},
      url = {https://doi.org/10.11648/j.ajae.20160302.12},
      eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ajae.20160302.12},
      abstract = {Many patents have suggested that spinning the aircraft wheel before touchdown would lessen tyre wear as indicated by landing smoke and rubber deposites on the runway caused by skidding wheel at the point of impact. In this paper, the required torque to spin the aircraft wheel at approach speed has been calculated using ANSYS Workbench CFX, which is used to determine the wheel aerodynamic forces developed by simulation of fluid flows in a virtual environment. The wheel has been tested against different wind speeds, and the aerodynamic forces for the spinning wheel are presented, which include; translational and rotational drags, lift created by vortex, and shaft rolling resistance.},
     year = {2016}
    }
    

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  • TY  - JOUR
    T1  - Determination of Required Torque to Spin Aircraft Wheel at Approach Using ANSYS CFX
    AU  - Abdurrhman A. Alroqi
    AU  - Weiji Wang
    Y1  - 2016/05/03
    PY  - 2016
    N1  - https://doi.org/10.11648/j.ajae.20160302.12
    DO  - 10.11648/j.ajae.20160302.12
    T2  - American Journal of Aerospace Engineering
    JF  - American Journal of Aerospace Engineering
    JO  - American Journal of Aerospace Engineering
    SP  - 13
    EP  - 23
    PB  - Science Publishing Group
    SN  - 2376-4821
    UR  - https://doi.org/10.11648/j.ajae.20160302.12
    AB  - Many patents have suggested that spinning the aircraft wheel before touchdown would lessen tyre wear as indicated by landing smoke and rubber deposites on the runway caused by skidding wheel at the point of impact. In this paper, the required torque to spin the aircraft wheel at approach speed has been calculated using ANSYS Workbench CFX, which is used to determine the wheel aerodynamic forces developed by simulation of fluid flows in a virtual environment. The wheel has been tested against different wind speeds, and the aerodynamic forces for the spinning wheel are presented, which include; translational and rotational drags, lift created by vortex, and shaft rolling resistance.
    VL  - 3
    IS  - 2
    ER  - 

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Author Information
  • Department of Engineering and Design, University of Sussex, Brighton, UK

  • Department of Engineering and Design, University of Sussex, Brighton, UK

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