Automation, Control and Intelligent Systems

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Determination of the Aerodynamic Characteristics of Flying Vehicles Using Method Large Eddy Simulation with Software ANSYS

Received: 08 September 2015    Accepted: 30 November 2015    Published: 22 December 2015
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Abstract

Nowadays, together with the huge development in information technology, the use of numerical method is no longer an obstacle. It provides a lot of advantages such as providing high precise solutions, reducing time and cost for designing and manufacturing flying vehicle models and dealing with extremely complex problems by using physical models compared to the usual analytical methods. The operation of airplanes represents a critical aerodynamic practical problem due to the wing. Interference this article presents a method to identify the aerodynamics coefficients of flying vehicles for isolate wing using software ANSYS. CFX and compares obtained results to the with those received by analytical method.

DOI 10.11648/j.acis.20150306.14
Published in Automation, Control and Intelligent Systems (Volume 3, Issue 6, December 2015)
Page(s) 118-123
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), 2024. Published by Science Publishing Group

Keywords

Aerodynamic Characteristics, Wing, Airfoil Section, Angle of Attack

References
[1] Ansys. CFX Release 12.0: ANSYS CFX-Solver Theory Guide.
[2] Ansys. Gambit Helps.
[3] Zakharchenko VF, et al., Determination of total aerodynamic characteristics of various configurations of aircraft. M: Publishing house of the MSTU. Bauman, 1993.
[4] AA Lebedev, Chernobrovkin LS Flight Dynamics: unmanned aerial vehicles. M: Mechanical Engineering, 1973.
[5] Process and research on the method of guidance a maneuvering target with scholastic prediction about its motion and with nonlinearities in the control circle” (A report on the scientific researching work)/MSTU named after Bauman. The supervisor: Pupkov K. A. The executors: Nguyen Quang Vinh, Bobkov A. V., Ustiuzanin A. D. / Moscow, 2006, 75 pages.
Author Information
  • Department of Radio-Electronic, Institute of Science and Technology, Cau Giay District, Hanoi, Vietnam

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  • APA Style

    Nguyen Quang Vinh. (2015). Determination of the Aerodynamic Characteristics of Flying Vehicles Using Method Large Eddy Simulation with Software ANSYS. Automation, Control and Intelligent Systems, 3(6), 118-123. https://doi.org/10.11648/j.acis.20150306.14

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    ACS Style

    Nguyen Quang Vinh. Determination of the Aerodynamic Characteristics of Flying Vehicles Using Method Large Eddy Simulation with Software ANSYS. Autom. Control Intell. Syst. 2015, 3(6), 118-123. doi: 10.11648/j.acis.20150306.14

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    AMA Style

    Nguyen Quang Vinh. Determination of the Aerodynamic Characteristics of Flying Vehicles Using Method Large Eddy Simulation with Software ANSYS. Autom Control Intell Syst. 2015;3(6):118-123. doi: 10.11648/j.acis.20150306.14

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  • @article{10.11648/j.acis.20150306.14,
      author = {Nguyen Quang Vinh},
      title = {Determination of the Aerodynamic Characteristics of Flying Vehicles Using Method Large Eddy Simulation with Software ANSYS},
      journal = {Automation, Control and Intelligent Systems},
      volume = {3},
      number = {6},
      pages = {118-123},
      doi = {10.11648/j.acis.20150306.14},
      url = {https://doi.org/10.11648/j.acis.20150306.14},
      eprint = {https://download.sciencepg.com/pdf/10.11648.j.acis.20150306.14},
      abstract = {Nowadays, together with the huge development in information technology, the use of numerical method is no longer an obstacle. It provides a lot of advantages such as providing high precise solutions, reducing time and cost for designing and manufacturing flying vehicle models and dealing with extremely complex problems by using physical models compared to the usual analytical methods. The operation of airplanes represents a critical aerodynamic practical problem due to the wing. Interference this article presents a method to identify the aerodynamics coefficients of flying vehicles for isolate wing using software ANSYS. CFX and compares obtained results to the with those received by analytical method.},
     year = {2015}
    }
    

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