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Design of a Small UAV Combined Between Flying-Wing and Quadrotor with XFRL5

Received: 13 April 2016     Accepted: 22 July 2016     Published: 3 September 2016
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Abstract

The design process of a product is a multi-step process of selection and assessment criteria to create a final product which meets all the needs of the practice. A small UAV combined between flying-wing and quadrotor is a very complex product, so the design process of this small UAV requires a thorough and circumspect review. The problem is how to optimize the design and to carry out the testing of the feasibility of design requirements with the lowest cost and time savings. For that reason, many tools of Multi-Fidelity Analysis for UAV such as XFLR5, XFoil… have been used to give considerable support for this design process. This research focusses mainly on the analysis/design of the configuration of a small UAV flying wing based on the performance at its cruise speed.

Published in International Journal of Transportation Engineering and Technology (Volume 2, Issue 4-1)

This article belongs to the Special Issue Experiments Researches in Aeronautical Engineering

DOI 10.11648/j.ijtet.s.2016020501.11
Page(s) 1-6
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

Small UAV Flying-wing, Quadrotor, XFRL5, Airfoil Selection for Small UAV

References
[1] S. Verling, J. Zilly, Modeling and Control of a VTOL Glider, Bachelor thesis, ETH, Zurich, 2013.
[2] M. Hochstenbach, C. Notteboom, Design and control of an unmanned aerial vehicle for autonomous parcel delivery with transition for vertical take-off to forward flight, Bachelor thesis, KU Leuven, Belgium, 2014.
[3] http://www.xflr5.com/xflr5.htm, XFLR5 V 6.09.
[4] M. Drela, “XFOIL: An analysis and design system for low Reynolds number airfoils”. In T. J. Mueller, editor, Low Reynolds Number Aerodynamics. Springer-Verlag, Jun 1989. http://web.mit.edu/drela/Public/web/xfoil
[5] Anh Bao DINH, Khanh Hieu NGO, Nhu Van Nguyen, An Efficient Low-Speed Airfoil Design Optimization Process Using Multi-Fidelity Analysis for UAV Flying Wing, Journal of Science & Technology Development, Vietnam National University, Ho Chi Minh City (accepted 05/2016).
[6] Ngo Khanh Hieu, Huynh Thien Loc, Airfoil Selection for Fixed Wing of Small Unmanned Aerial Vehicles, AETA2015: Recent Advanced in Electrical Engineering and Related Sciences, Ho Chi Minh City, Vietnam, 2015.
[7] Michael S. Selig, Christopher A. Lyon, Philippe Giguère, Cameron P. Ninham, and James J. Guglielmo, Summary of Low Speed airfoil data Volume 2, Department of Aerospace Engineering, University of Illinois at Urbana-Champaign, 1996.
[8] Christopher A. Lyon, Andy P. Broeren, Philippe Giguère, Ashok Gopalarathnam, and Michael S. Selig, Summary of Low Speed airfoil data Volume 3, Department ofAerospace Engineering, University of Illinois at Urbana-Champaign, 1997.
[9] Gregory A Williamson, Bryan D. McGranahan, Benjamin A. Broughton, Robert W. Deters, John B. Brandt and M. S. Selig, Summary of Low Speed airfoil data Volume 5, Department ofAerospace Engineering, University of Illinois at Urbana-Champaign, 2012.
[10] Ngo Khanh Hieu, Bui Khac Huy, Electric RC Model Airplane carrying payload up to 300 grams: Design and Manufacture, the 4th AUN/SEED-Net Regional Conference in Mechanical and Aerospace Technology, Ho Chi Minh City, Vietnam, 2012.
[11] Robert C. Nelson, Flight Stability and Automatic Control, McGraw-Hill Education, 2nd edition, 1997.
[12] Roskam, Method for Estimating Drag Polars of Subsonic Airplanes, Aviation and Engineering corporation, 1983.
Cite This Article
  • APA Style

    Ngo Khanh Hieu, Pham Quang Vinh, Dinh Anh Bao. (2016). Design of a Small UAV Combined Between Flying-Wing and Quadrotor with XFRL5. International Journal of Transportation Engineering and Technology, 2(4-1), 1-6. https://doi.org/10.11648/j.ijtet.s.2016020501.11

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    ACS Style

    Ngo Khanh Hieu; Pham Quang Vinh; Dinh Anh Bao. Design of a Small UAV Combined Between Flying-Wing and Quadrotor with XFRL5. Int. J. Transp. Eng. Technol. 2016, 2(4-1), 1-6. doi: 10.11648/j.ijtet.s.2016020501.11

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    AMA Style

    Ngo Khanh Hieu, Pham Quang Vinh, Dinh Anh Bao. Design of a Small UAV Combined Between Flying-Wing and Quadrotor with XFRL5. Int J Transp Eng Technol. 2016;2(4-1):1-6. doi: 10.11648/j.ijtet.s.2016020501.11

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  • @article{10.11648/j.ijtet.s.2016020501.11,
      author = {Ngo Khanh Hieu and Pham Quang Vinh and Dinh Anh Bao},
      title = {Design of a Small UAV Combined Between Flying-Wing and Quadrotor with XFRL5},
      journal = {International Journal of Transportation Engineering and Technology},
      volume = {2},
      number = {4-1},
      pages = {1-6},
      doi = {10.11648/j.ijtet.s.2016020501.11},
      url = {https://doi.org/10.11648/j.ijtet.s.2016020501.11},
      eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ijtet.s.2016020501.11},
      abstract = {The design process of a product is a multi-step process of selection and assessment criteria to create a final product which meets all the needs of the practice. A small UAV combined between flying-wing and quadrotor is a very complex product, so the design process of this small UAV requires a thorough and circumspect review. The problem is how to optimize the design and to carry out the testing of the feasibility of design requirements with the lowest cost and time savings. For that reason, many tools of Multi-Fidelity Analysis for UAV such as XFLR5, XFoil… have been used to give considerable support for this design process. This research focusses mainly on the analysis/design of the configuration of a small UAV flying wing based on the performance at its cruise speed.},
     year = {2016}
    }
    

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    AB  - The design process of a product is a multi-step process of selection and assessment criteria to create a final product which meets all the needs of the practice. A small UAV combined between flying-wing and quadrotor is a very complex product, so the design process of this small UAV requires a thorough and circumspect review. The problem is how to optimize the design and to carry out the testing of the feasibility of design requirements with the lowest cost and time savings. For that reason, many tools of Multi-Fidelity Analysis for UAV such as XFLR5, XFoil… have been used to give considerable support for this design process. This research focusses mainly on the analysis/design of the configuration of a small UAV flying wing based on the performance at its cruise speed.
    VL  - 2
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Author Information
  • Department of Aerospace Engineering, Ho Chi Minh City University of Technology, Ho Chi Minh City, Vietnam

  • Department of Aerospace Engineering, Ho Chi Minh City University of Technology, Ho Chi Minh City, Vietnam

  • Department of Aerospace Engineering, Ho Chi Minh City University of Technology, Ho Chi Minh City, Vietnam

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