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Research on Coupling of Low Speed Straight-Flow Wind Tunnel Based on Ansys Workbench

Received: 12 September 2017     Published: 14 September 2017
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Abstract

Introduction of research on coupling of low speed straight-flow wind tunnel based on ANSYS Workbench. Wind tunnel is a most important test method of aerodynamics research, in which the air velocity field and pressure field determine the test research level. A computational fluid dynamics simulation based on ANSYS Fluent is conducted on wind tunnel, together with a coupling analysis of the fluid and wind tunnel structure, which helps us make further research on wind tunnel’s air field and structure. This work contributes to better operating of test research and wind tunnel optimization design.

Published in Science Discovery (Volume 5, Issue 5)
DOI 10.11648/j.sd.20170505.23
Page(s) 380-384
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

Straight-Flow Wind Tunnel, Low Speed Wind Tunnel, Fluid-Solid Coupling, ANSYS Workbench

References
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Cite This Article
  • APA Style

    Zhang Yifei, Qiu Rongkai, Shen Jiang. (2017). Research on Coupling of Low Speed Straight-Flow Wind Tunnel Based on Ansys Workbench. Science Discovery, 5(5), 380-384. https://doi.org/10.11648/j.sd.20170505.23

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    ACS Style

    Zhang Yifei; Qiu Rongkai; Shen Jiang. Research on Coupling of Low Speed Straight-Flow Wind Tunnel Based on Ansys Workbench. Sci. Discov. 2017, 5(5), 380-384. doi: 10.11648/j.sd.20170505.23

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    AMA Style

    Zhang Yifei, Qiu Rongkai, Shen Jiang. Research on Coupling of Low Speed Straight-Flow Wind Tunnel Based on Ansys Workbench. Sci Discov. 2017;5(5):380-384. doi: 10.11648/j.sd.20170505.23

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  • @article{10.11648/j.sd.20170505.23,
      author = {Zhang Yifei and Qiu Rongkai and Shen Jiang},
      title = {Research on Coupling of Low Speed Straight-Flow Wind Tunnel Based on Ansys Workbench},
      journal = {Science Discovery},
      volume = {5},
      number = {5},
      pages = {380-384},
      doi = {10.11648/j.sd.20170505.23},
      url = {https://doi.org/10.11648/j.sd.20170505.23},
      eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.sd.20170505.23},
      abstract = {Introduction of research on coupling of low speed straight-flow wind tunnel based on ANSYS Workbench. Wind tunnel is a most important test method of aerodynamics research, in which the air velocity field and pressure field determine the test research level. A computational fluid dynamics simulation based on ANSYS Fluent is conducted on wind tunnel, together with a coupling analysis of the fluid and wind tunnel structure, which helps us make further research on wind tunnel’s air field and structure. This work contributes to better operating of test research and wind tunnel optimization design.},
     year = {2017}
    }
    

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  • TY  - JOUR
    T1  - Research on Coupling of Low Speed Straight-Flow Wind Tunnel Based on Ansys Workbench
    AU  - Zhang Yifei
    AU  - Qiu Rongkai
    AU  - Shen Jiang
    Y1  - 2017/09/14
    PY  - 2017
    N1  - https://doi.org/10.11648/j.sd.20170505.23
    DO  - 10.11648/j.sd.20170505.23
    T2  - Science Discovery
    JF  - Science Discovery
    JO  - Science Discovery
    SP  - 380
    EP  - 384
    PB  - Science Publishing Group
    SN  - 2331-0650
    UR  - https://doi.org/10.11648/j.sd.20170505.23
    AB  - Introduction of research on coupling of low speed straight-flow wind tunnel based on ANSYS Workbench. Wind tunnel is a most important test method of aerodynamics research, in which the air velocity field and pressure field determine the test research level. A computational fluid dynamics simulation based on ANSYS Fluent is conducted on wind tunnel, together with a coupling analysis of the fluid and wind tunnel structure, which helps us make further research on wind tunnel’s air field and structure. This work contributes to better operating of test research and wind tunnel optimization design.
    VL  - 5
    IS  - 5
    ER  - 

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Author Information
  • Equipment Design and Instrument Research Institute, China Aerodynamics Research and Development Center, Mianyang, China

  • Equipment Design and Instrument Research Institute, China Aerodynamics Research and Development Center, Mianyang, China

  • Equipment Design and Instrument Research Institute, China Aerodynamics Research and Development Center, Mianyang, China

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